US20180327067A1 - Outboard motor and sealing structure for divisible engine cover used therefor - Google Patents
Outboard motor and sealing structure for divisible engine cover used therefor Download PDFInfo
- Publication number
- US20180327067A1 US20180327067A1 US15/964,137 US201815964137A US2018327067A1 US 20180327067 A1 US20180327067 A1 US 20180327067A1 US 201815964137 A US201815964137 A US 201815964137A US 2018327067 A1 US2018327067 A1 US 2018327067A1
- Authority
- US
- United States
- Prior art keywords
- bottom portion
- boundary
- side bottom
- seal
- engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000007789 sealing Methods 0.000 title claims abstract description 76
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 79
- 238000003780 insertion Methods 0.000 claims description 20
- 230000037431 insertion Effects 0.000 claims description 20
- 238000001125 extrusion Methods 0.000 claims description 8
- 230000008878 coupling Effects 0.000 description 17
- 238000010168 coupling process Methods 0.000 description 17
- 238000005859 coupling reaction Methods 0.000 description 17
- 229920001971 elastomer Polymers 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 239000011347 resin Substances 0.000 description 5
- 229920005989 resin Polymers 0.000 description 5
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000000498 cooling water Substances 0.000 description 1
- 238000010070 extrusion (rubber) Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 229920002725 thermoplastic elastomer Polymers 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H20/00—Outboard propulsion units, e.g. outboard motors or Z-drives; Arrangements thereof on vessels
- B63H20/32—Housings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
- F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
- F02B61/045—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers for marine engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/16—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines characterised by use in vehicles
- F02M35/165—Marine vessels; Ships; Boats
- F02M35/167—Marine vessels; Ships; Boats having outboard engines; Jet-skis
- F02M35/168—Marine vessels; Ships; Boats having outboard engines; Jet-skis with means, e.g. valves, to prevent water entry
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H20/00—Outboard propulsion units, e.g. outboard motors or Z-drives; Arrangements thereof on vessels
- B63H20/24—Arrangements, apparatus and methods for handling exhaust gas in outboard drives, e.g. exhaust gas outlets
- B63H20/245—Exhaust gas outlets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H20/00—Outboard propulsion units, e.g. outboard motors or Z-drives; Arrangements thereof on vessels
- B63H20/32—Housings
- B63H2020/323—Gear cases
Definitions
- the present invention relates to an outboard motor and a sealing structure for a divisible engine cover used therefor.
- the outboard motor described in Japanese Unexamined Patent Application Publication No. H6-234393 includes a motor cowl covering an engine, the motor cowl being divisible into an upper motor cover and a lower motor cover.
- the boundary between the lower end of the upper motor cover and the upper end of the lower motor cover is sealed with a cover seal that is annular in plan view.
- the lower motor cover is divisible into a first cover portion and a second cover portion.
- the motor cowl described in Japanese Unexamined Patent Application Publication No. H6-234393 has a boundary spanning three parts of the upper motor cover, the first cover portion, and the second cover portion and another boundary continuous with the boundary and existing between the two parts of the first cover portion and the second cover portion.
- annular, i.e., simply shaped, cover seal disclosed in Japanese Unexamined Patent Application Publication No. H6-234393 it is difficult to seal these boundaries without leakage, and external water may leak through the boundaries and enter into the engine cover. When the water within the engine cover enters into the engine, a problem may occur with the engine.
- a preferred embodiment of the present invention provides an outboard motor including an engine, an engine cover including at least a first cover, a second cover, and a third cover that cover the engine, and a seal.
- the engine cover includes a first boundary spanning three portions of the first cover, the second cover, and the third cover and a second boundary between two of the three portions and continuous with the first boundary.
- the seal integrally includes a three-part seal that seals the first boundary and a two-part seal with a structure different from that of the three-part seal and that seals the second boundary.
- the engine cover is divisible into at least the first cover, the second cover, and the third cover, has the first boundary spanning three portions of the three covers and the second boundary between two of the three portions and continuous with the first boundary.
- the seal integrally includes the three-part seal and the two-part seal, which seal the first boundary and the second boundary and have respective different structures.
- the seal seals the first boundary and the second boundary with the three-part seal sealing the first boundary and the two-part seal sealing the second boundary. This significantly reduces or prevents external water from leaking through the first boundary and the second boundary, which are boundaries between the covers of the divisible engine cover, and entering into the engine.
- the three-part seal may be a molded article and the two-part seal may be an extrusion molded article.
- a clearance gap in the complex shaped first boundary spanning the three portions is filled with the molded three-part seal and a clearance gap in the second boundary spanning the two portions is filled with the extrusion molded two-part seal. This allows the seal to seal the first boundary and the second boundary.
- a preferred embodiment of the present invention provides an outboard motor including an engine, a mount on which the engine is mounted, an engine cover, and a sealing structure for the engine cover.
- the engine cover includes a top portion opposing the engine from above, a front bottom portion opposing the engine from the front, and a side bottom portion opposing the engine from the side.
- the front bottom portion is located at a position lower than a position of the top portion
- the side bottom portion is located at a position lower than the position of the top portion and rearward of the front bottom portion.
- the engine cover is coupled to the mount through the front bottom portion and the side bottom portion.
- the sealing structure includes a first seal.
- the first seal integrally includes a first portion, a second portion, and a third portion extending from the first portion to the second portion.
- the first portion seals the boundary between the top portion, the front bottom portion, and the side bottom portion.
- the second portion seals the boundary between the front bottom portion, the mount, and the side bottom portion.
- the third portion
- an engine cover which is divisible into three or more covers including at least the top portion, the front bottom portion, and the side bottom portion, includes a boundary between the top portion, the front bottom portion, and the side bottom portion and a boundary between the front bottom portion, the mount, and the side bottom portion.
- the first seal of the sealing structure seals the boundary between the top portion, the front bottom portion, and the side bottom portion with the first portion; seals the boundary between the front bottom portion, the mount, and the side bottom portion with the second portion; and seals the other boundary extending between these boundaries with the third portion.
- This structure provides desirable sealing characteristics for a divisible engine cover having such a complex structure. This significantly reduces or prevents external water from leaking through the boundaries between the multiple covers of the divisible engine cover and entering into the engine.
- the first portion may be located at a position higher than a position of the second portion, and an upper end of the front bottom portion may include an opposing portion that opposes an upper end of the side bottom portion from within the engine cover.
- the first portion integrally includes an inner portion and an outer portion.
- the inner portion is at least partially located between the opposing portion and the upper end of the side bottom portion.
- the outer portion extends through the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion so as to be located on the outer surface of the upper end of the front bottom portion.
- the inner portion includes a water storage groove adjacent to the outer portion and opposing the side bottom portion.
- the first portion seals the boundary between the opposing portion in the upper end of the front bottom portion and the upper end of the side bottom portion with the inner portion and seals the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion with the outer portion.
- This structure provides desirable sealing characteristics at the boundary between the upper end of the front bottom portion and the upper end of the side bottom portion. This significantly reduces or prevents external water from leaking through the boundary between the upper end of the side bottom portion and the upper end of the front bottom portion and entering into the engine.
- the inner portion may include an upper rib protruding toward the upper end of the side bottom portion and extending rearward from the upper end of the water storage groove.
- water within the water storage groove will be blocked by the upper rib from scattering upward within the engine cover to reach the engine, which further significantly reduces or prevents water from entering into the engine.
- a drainage hole may be provided in a lower portion of the engine cover or the mount, and the inner portion may include a guide extending rearward from the lower end of the water storage groove to guide water within the water storage groove to the drainage hole.
- water within the water storage groove is guided through the guide to the drainage hole and discharged out of the engine cover, which further significantly reduces or prevents water from entering into the engine.
- an insertion hole through which a fastening member coupling the opposing portion and the side bottom portion is inserted, may be provided in a penetrating manner in a portion of the inner portion located between the upper rib and the guide.
- the water is blocked by the upper rib from scattering upward to reach the engine and also is guided through the guide to the drainage hole to be discharged out of the engine cover. This further significantly reduces or prevents water from entering into the engine.
- the sealing structure may further include a second seal that seals the boundary between the top portion and the front bottom portion and the boundary between the top portion and the side bottom portion.
- the second seal may surround a portion of the outer portion located between the second seal and the front bottom portion.
- the second seal provides desirable sealing characteristics at the boundary between the top portion and the front bottom portion and the boundary between the top portion and the side bottom portion. This significantly reduces or prevents external water from leaking through these boundaries and entering into the engine.
- the second seal surrounds a portion of the outer portion, which seals the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion in the first seal, between the second seal and the front bottom portion. This causes the first seal and the second seal to be continuous with each other. Since the boundary between the top portion, the front bottom portion, and the side bottom portion is thus sealed by both the first seal and the second seal, this structure provides desirable sealing characteristics at the boundary. This significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- the sealing structure may further include a third seal that seals the boundary between the mount and the front bottom portion and the boundary between the mount and the side bottom portion.
- the second portion includes a sealing surface that adheres to the third seal from the front at the boundary between the front bottom portion, the mount, and the side bottom portion.
- the third seal provides desirable sealing characteristics at the boundary between the mount and the front bottom portion and the boundary between the mount and the side bottom portion. This significantly reduces or prevents external water from leaking through these boundaries and entering into the engine.
- the sealing surface of the second portion adheres tightly to the third seal from the front at the boundary between the front bottom portion, the mount, and the side bottom portion to seal the boundary. This causes the first seal and the third seal to be continuous with each other. Since the boundary is thus sealed by both the first seal and the third seal, desirable sealing characteristics at the boundary are achieved. This significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- a longitudinally extending positioning groove may be provided in the second portion, and the front bottom portion may include a positioning portion fitted into the positioning groove.
- the second portion is preferably positioned laterally to seal the boundary between the front bottom portion, the mount, and the side bottom portion with the lateral position being stabilized.
- This structure provides desirable sealing characteristics at the boundary and significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- the first portion and the second portion may be molded articles and the third portion may be an extrusion molded article.
- the first seal integrally includes the first portion, the second portion, and the third portion.
- the engine cover may be divisible into the top portion, the front bottom portion, and a pair of the left and right side bottom portions opposing the engine, respectively, from the left and the right.
- the sealing structure includes a pair of the left and right first seals.
- the sealing structure may further include a fourth seal that seals the boundary between the pair of side bottom portions.
- the divisible engine cover has a more complex structure due to it being divided into four or more covers of the top portion, the front bottom portion, and the pair of left and right side bottom portions.
- the pair of left and right first seals correspond to the pair of left and right side bottom portions.
- the left first seal seals the boundary between the top portion, the front bottom portion, and the left side bottom portion with the first portion and seals the boundary between the front bottom portion, the mount, and the left side bottom portion with the second portion.
- the left first seal seals the other boundary extending between these boundaries with the third portion.
- the right first seal seals the boundary between the top portion, the front bottom portion, and the right side bottom portion with the first portion and seals the boundary between the front bottom portion, the mount, and the right side bottom portion with the second portion.
- the right first seal seals the other boundary extending between these boundaries with the third portion.
- the fourth seal seals the boundary between the pair of side bottom portions.
- FIG. 1 is a schematic perspective view of an outboard motor according to a preferred embodiment of the present invention.
- FIG. 2 is a schematic exploded perspective view of an upper portion of an outboard motor main body in the outboard motor.
- FIG. 3 is a perspective view of a sealing structure for a divisible engine cover in the outboard motor main body.
- FIG. 4 is a schematic cross-sectional view showing a natural state prior to deformation of a fourth seal in the sealing structure.
- FIG. 5 is a schematic horizontal cross-sectional view of the engine cover in the region A of FIG. 3 .
- FIG. 6 is a schematic cross-sectional view showing a natural state prior to deformation of a third seal in the sealing structure.
- FIG. 7 is a schematic vertical cross-sectional view of the engine cover in the region B of FIG. 3 .
- FIG. 8 is a schematic cross-sectional view showing a natural state prior to deformation of a second lower seal in the sealing structure.
- FIG. 9 is a schematic cross-sectional view showing a natural state prior to deformation of a second upper seal in the sealing structure.
- FIG. 10 is a schematic vertical cross-sectional view of the engine cover in the region C of FIG. 3 .
- FIG. 11 is a schematic perspective view of a first seal in the sealing structure.
- FIG. 12 is a schematic cross-sectional view showing a natural state prior to deformation of a third portion in the first seal.
- FIG. 13 is a schematic left side view of the first seal and its periphery.
- FIG. 14 is an end view of a cut portion along the line A-A in FIG. 13 .
- FIG. 15 is a schematic perspective view of the first portion of the first seal and its periphery.
- FIG. 16 is an end view of a cut portion along the line B-B in FIG. 13 .
- FIG. 17 is a cross-sectional view taken along the line C-C in FIG. 13 .
- FIG. 18 is an end view of a cut portion along the line D-D in FIG. 13 .
- FIG. 19 is a cross-sectional view taken along the line E-E in FIG. 18 .
- FIG. 20 is an end view of a cut portion along the line F-F in FIG. 13 .
- FIG. 1 is a schematic front perspective view of an outboard motor 1 according to a preferred embodiment of the present invention.
- the outboard motor 1 shown in FIG. 1 is in a basic posture.
- the rotation axis 2 A of a propeller 2 in the outboard motor 1 extends both horizontally and in a front to back direction.
- the front to back direction, the lateral direction, and the vertical direction in the following description correspond, respectively, to the front to back direction, the lateral direction, and the vertical direction when the outboard motor 1 is in the basic posture.
- the outboard motor 1 includes an outboard motor main body 10 and an installation mechanism (not shown) arranged to install the outboard motor main body 10 on a hull (not shown). Supported by the installation mechanism, the outboard motor main body 10 is turned vertically about a laterally extending horizontal axis 11 and also turned laterally about a vertically extending vertical axis 12 .
- the outboard motor main body 10 includes the propeller 2 , an engine 13 , a drive shaft 14 , a propeller shaft 15 , a gear mechanism 16 , a casing 17 , a mount 18 (see FIG. 2 below), and an engine cover 19 .
- the engine 13 is, for example, an internal combustion engine or an electric motor.
- the engine 13 is preferably an internal combustion engine with a crankshaft (not shown) incorporated therein arranged to rotate about a vertically extending crank axis.
- the drive shaft 14 is coupled to a lower end of the crankshaft (not shown) of the engine 13 and extends downward.
- the propeller shaft 15 extends in in a front to back direction at a position lower than that of the lower end of the drive shaft 14 .
- the gear mechanism 16 couples the lower end of the drive shaft 14 and a front end of the propeller shaft 15 .
- the propeller 2 is attached to a rear end of the propeller shaft 15 .
- the rotation of the drive shaft 14 with the driving of the engine 13 is transmitted by the gear mechanism 16 to the propeller shaft 15 .
- the rotation axis 2 A of the propeller 2 coincides with the central axis of the propeller shaft 15 .
- the rotation of the propeller 2 generates a propulsive force for forward or rearward movement of the hull.
- the casing 17 is a vertically extending hollow body housing the drive shaft 14 , the propeller shaft 15 , and the gear mechanism 16 therein.
- the propeller shaft 15 and the gear mechanism 16 are housed in a lower case 17 A that is a lower end of the casing 17 .
- the propeller 2 is located outside the lower case 17 A.
- FIG. 2 is a schematic exploded perspective view of an upper portion of the outboard motor main body 10 .
- the mount 18 is a so-called exhaust guide preferably made of metal such as aluminum and having a plate shape.
- the mount 18 is installed in an upper end of the casing 17 in a manner closing the interior space of the casing 17 from above.
- the upper surface of the mount 18 preferably has a rectangular or substantially rectangular shape elongated in the front to back direction.
- the engine 13 is mounted on the upper surface of the mount 18 .
- the outer edge 18 A of the upper surface of the mount 18 defines the outline of the mount 18 in plan view and protrudes outwardly from the engine 13 around the entire circumference.
- An insertion hole 18 B, an exhaust hole 18 C located, for example, rearward of the insertion hole 18 B, and two drainage holes 18 D located, for example, on each of the left and right sides of the exhaust hole 18 C are provided in the upper surface of the mount 18 .
- the insertion hole 18 B, the exhaust hole 18 C, and the drainage holes 18 D penetrate through the mount 18 vertically.
- the drive shaft 14 is inserted through the insertion hole 18 B.
- Exhaust gas from the engine 13 is discharged through the exhaust hole 18 C and the interior of the casing 17 out of the outboard motor main body 10 .
- Water, if on the upper surface of the mount 18 falls through the drainage holes 18 D and the interior of the casing 17 to be discharged out of the outboard motor main body 10 .
- the mount 18 may include a portion of a flow path for cooling water that cools the engine 13 or lubricant that lubricates the engine 13 .
- the engine cover 19 preferably has a box shape and is located at a position higher than that of the casing 17 to cover the engine 13 (see FIG. 1 ).
- the engine cover 19 is vertically divisible into a top portion 25 exemplifying a first cover and a bottom portion 26 .
- the bottom portion 26 defining a lower portion of the engine cover 19 is divisible into at least a front bottom portion 27 exemplifying a second cover and a side bottom portion 28 exemplifying a third cover.
- the top portion 25 is made of, for example, resin and preferably has a box shape.
- the top portion 25 includes an opening (not shown) that opens the interior space thereof downward.
- the resin is preferably, for example, a thermosetting resin.
- the lower edge 25 A of the top portion 25 has a continuous annular shape to define the opening.
- the front bottom portion 27 is made of, for example, metal such as aluminum and integrally includes a horizontal portion 27 A and a vertical portion 27 B.
- the horizontal portion 27 A preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the vertical direction.
- the horizontal portion 27 A preferably has a semicircular or substantially semicircular shape in plan view.
- the front edge of the horizontal portion 27 A is thus curved in an arcuate shape bulging forward.
- the rear edge of the horizontal portion 27 A is also curved in an arcuate shape bulging forward.
- the rear edge of the horizontal portion 27 A includes a fitting groove 27 C extending in a curved manner along the rear edge.
- the fitting groove 27 C is recessed forward and opens rearward.
- drainage holes 27 D are provided in a manner vertically penetrating through the horizontal portion 27 A.
- the vertical portion 27 B preferably has a plate shape curved along the front edge of the horizontal portion 27 A and extending upward.
- the front surface of the vertical portion 27 B defines a portion of the outer surface of the engine cover 19 .
- the portion of the vertical portion 27 B higher than the horizontal step 27 E includes an upper end 27 G of the front bottom portion 27 .
- the front surface of the upper end 27 G is offset rearward by one step from the portion of the front surface of the vertical portion 27 B surrounded by the horizontal step 27 E and the pair of vertical steps 27 F.
- Opposing portions 27 H are provided integrally at the respective lateral ends of the upper end 27 G.
- a screw hole 27 I is provided in the left surface of the left opposing portion 27 H.
- a screw hole 27 I is also provided in the right surface of the right opposing portion 27 H.
- the portion of the vertical portion 27 B rearward of each vertical step 27 F will be referred to as a rear portion 27 J.
- the upper end edge of the rear portion 27 J is inclined so as to descend as it extends rearward.
- the side bottom portion 28 is made of, for example, resin and includes a pair of left and right portions. Of the pair of left and right side bottom portions 28 , the left side bottom portion 28 will be referred to as a side bottom portion 28 L, while the right side bottom portion 28 will be referred to as a side bottom portion 28 R.
- the side bottom portion 28 L and the side bottom portion 28 R are preferably laterally symmetric.
- Each side bottom portion 28 integrally includes a plate-shaped main body 28 A extending in a front to back and vertical direction and an extended portion 28 B extending in a manner bent from the rear end of the main body 28 A toward the other side bottom portion 28 .
- the pair of side bottom portions 28 are coupled through a right end of the extended portion 28 B of the side bottom portion 28 L and a left end of the extended portion 28 B of the side bottom portion 28 R.
- the right end of the extended portion 28 B of the side bottom portion 28 L and the left end of the extended portion 28 B of the side bottom portion 28 R will each be referred to as a coupling 28 C.
- the left surface of the main body 28 A and the rear surface of the extended portion 28 B defines the outer surface of the side bottom portion 28 L and a portion of the outer surface of the engine cover 19 .
- the right surface of the main body 28 A and the front surface of the extended portion 28 B define the inner surface of the side bottom portion 28 L and a portion of the inner surface of the engine cover 19 .
- the right surface of the main body 28 A and the rear surface of the extended portion 28 B define the outer surface of the side bottom portion 28 R and a portion of the outer surface of the engine cover 19 .
- the left surface of the main body 28 A and the front surface of the extended portion 28 B define the inner surface of the side bottom portion 28 R and a portion of the inner surface of the engine cover 19 .
- a step 28 D extends from the front end of the main body 28 A to the coupling 28 C.
- the portion of each side bottom portion 28 higher than the step 28 D is an upper end 28 E of the side bottom portion 28 .
- the outer surface of the upper end 28 E is offset by one step inside the engine cover 19 farther than the portion of the outer surface of the side bottom portion 28 lower than the step 28 D.
- a recess 28 F is recessed inward of the engine cover 19 .
- a bottom portion 28 G of the recess 28 F is raised in a convex shape on the inner surface of the side bottom portion 28 .
- the bottom portion 28 G is provided with an insertion hole 28 H penetrating laterally through the bottom portion 28 G.
- each side bottom portion 28 On the inner surface of each side bottom portion 28 , there is integrally provided an upper rib 28 I protruding inward of the engine cover 19 and extending from the lower end of the bottom portion 28 G of the recess 28 F to the lower end of the coupling 28 C.
- a lower rib 28 J On the inner surface of each side bottom portion 28 , there is integrally provided a lower rib 28 J extending from a location rearward of the bottom portion 28 G to the lower end of the coupling 28 C.
- the lower rib 28 J is located below a portion of the upper rib 28 I and extends parallel or substantially parallel with the upper rib 28 I to the lower end of the coupling 28 C.
- a fitting groove 28 K is provided between the upper rib 28 I and the lower rib 28 J.
- the fitting groove 28 K extends from a position rearward of the bottom portion 28 G to the lower end of the coupling 28 C.
- the portion of the upper rib 28 I located forward of the fitting groove 28 K and extending to the lower end of the recess 28 F will be referred to as an extended section 28 M.
- the lower rib 28 J does not exist below the extended section 28 M.
- FIG. 1 Assembly of the divisible engine cover 19 will be described with reference also to FIG. 1 .
- an operator brings the front bottom portion 27 closer to the mount 18 and fits the front portion of the outer edge 18 A of the mount 18 into the fitting groove 27 C in the horizontal portion 27 A of the front bottom portion 27 from behind.
- This causes the front bottom portion 27 to be coupled to the mount 18 .
- the rear edge of the horizontal portion 27 A is provided with a fixed portion 27 P protruding rearward to overlap the front end of the mount 18 from above.
- a fastening member (not shown) such as a bolt is assembled into a screw hole 18 E in the front end of the mount 18 through an insertion hole 27 Q defined in the fixed portion 27 P such that the mount 18 and the front bottom portion 27 are fixed to each other.
- the operator arranges the pair of side bottom portions 28 at a position rearward of the front bottom portion 27 and sandwiches the mount 18 bilaterally with the side bottom portions 28 until the couplings 28 C are coupled to each other.
- the left portion of the outer edge 18 A of the mount 18 fits into the fitting groove 28 K (not shown) in the side bottom portion 28 L from the right, while the right portion of the outer edge 18 A fits into the fitting groove 28 K in the side bottom portion 28 R from the left.
- This causes the side bottom portions 28 to be coupled to the mount 18 .
- the side bottom portions 28 and the mount 18 may be fixed using a fastening member such as a bolt if needed.
- the front portion of the main body 28 A of the side bottom portion 28 L covers the left rear portion 27 J of the vertical portion 27 B of the front bottom portion 27 from the left.
- the front portion of the main body 28 A of the side bottom portion 28 R covers the right rear portion 27 J of the main body 28 A from the right.
- the left and right opposing portions 27 H in the upper end 27 G of the front bottom portion 27 are opposed from within the engine cover 19 to the bottom portions 28 G of the recesses 28 F in the upper ends 28 E of the side bottom portions 28 located at laterally corresponding positions.
- the insertion holes 28 H in the bottom portions 28 G and the screw holes 27 I in the opposing portions 27 H are aligned with each other.
- the horizontal step 27 E of the vertical portion 27 B of the front bottom portion 27 and the steps 28 D of the side bottom portions 28 are connected to define one annular body (see FIG. 1 ).
- the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surfaces of the upper ends 28 E of the side bottom portions 28 are also connected to define one annular body.
- the fitting groove 27 C in the horizontal portion 27 A of the front bottom portion 27 and the fitting grooves 28 K in the side bottom portions 28 are also connected to define one annular body.
- the upper end edges of the left and right rear portions 27 J of the vertical portion 27 B are opposed from below to the extended sections 28 M of the side bottom portions 28 located at laterally corresponding positions.
- the top portion 25 may be fixed to the front bottom portion 27 and the side bottom portions 28 using a fastening member such as a bolt if needed.
- the front bottom portion 27 is located at a position lower than that of the top portion 25 and the pair of side bottom portions 28 are located at a position lower than that of the top portion 25 and rearward of the front bottom portion 27 (see FIG. 1 ).
- the engine 13 mounted on the mount 18 is opposed at least upward to the top portion 25 and opposed forward to at least the vertical portion 27 B of the front bottom portion 27 .
- the engine 13 is also opposed sideward, that is, leftward and rightward to at least the main body portions 28 A and opposed rearward to at least the extended portions 28 B of the pair of side bottom portions 28 .
- the engine cover 19 may further include a rear panel 30 that covers the extended portions 28 B of the pair of side bottom portions 28 from behind.
- the multiple boundaries in the engine cover 19 are, for example, one between the top portion 25 and the front bottom portion 27 and ones between the two portions of the front bottom portion 27 and each side bottom portion 28 (referred to as a second boundary B 2 ; see FIG. 20 below).
- the boundary between the top portion 25 and each side bottom portion 28 and the boundary between the pair of side bottom portions 28 also exist as boundaries in the engine cover 19 .
- An air-intake structure (not shown) of the engine 13 including, for example, an air-intake box and a throttle body is located at a position within the engine cover 19 higher than those of the boundary between the top portion 25 and the front bottom portion 27 and the boundary between the top portion 25 and each side bottom portion 28 .
- the boundary spanning the three portions of the top portion 25 , the front bottom portion 27 , and each side bottom portion 28 (referred to as a first boundary B 1 ; see FIG. 1 ) also exists as a boundary in the engine cover 19 .
- the first boundary B 1 and the second boundary B 2 are continuous with each other.
- the outboard motor 1 includes a sealing structure 40 that seals all of these boundaries.
- FIG. 3 is a perspective view of the sealing structure 40 .
- the sealing structure 40 includes a first seal 41 , a second seal 42 , a third seal 43 , and a fourth seal 44 .
- the fourth seal 44 , the third seal 43 , the second seal 42 , and the first seal 41 will hereinafter be described in this order.
- the fourth seal 44 preferably has a vertically extending columnar shape between the couplings 28 C of the pair of side bottom portions 28 .
- the cross-section of the fourth seal 44 in the direction perpendicular or substantially perpendicular to the direction in which the fourth seal 44 extends has a structure shown in FIG. 4 at any position in the extending direction of the fourth seal 44 .
- the fourth seal 44 includes a core portion 44 A made of, for example, metal such as iron and an elastic portion 44 B made of, for example, rubber and coating the entire core portion 44 A.
- the core portion 44 A preferably has a U-shaped or substantially U-shaped cross-section and the elastic portion 44 B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to the core portion 44 A.
- the rubber is, for example, a thermoplastic elastomer.
- the elastic portion 44 B includes a tongue-shaped first protrusion 44 D protruding into a concave space 44 C sandwiched between the core portion 44 A.
- the first protrusion 44 D is provided on one of a pair of flat regions of the inner surface of the elastic portion 44 B extending parallel or substantially parallel to each other with the space 44 C sandwiched therebetween and protrudes in a manner away from an opening 44 E of the space 44 C.
- Multiple first protrusions 44 D may be provided and, in this preferred embodiment, two first protrusions 44 D are arranged parallel or substantially parallel to each other.
- the elastic portion 44 B includes a second protrusion 44 F protruding in a direction away from the opening 44 E of the space 44 C.
- the second protrusion 44 F is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from the opening 44 E.
- the curved portion of the core portion 44 A is positioned between the space 44 C and the second protrusion 44 F.
- FIG. 5 is a schematic horizontal cross-sectional view of the engine cover 19 in the region A of FIG. 3 .
- the coupling 28 C of each side bottom portion 28 preferably has a columnar shape protruding forward from the rear surface of the extended portion 28 B and extending in the vertical direction.
- a vertically extending groove 28 N is provided in a region opposing the other coupling 28 C.
- the grooves 28 N of each other's side bottom portions 28 abut each other and are integral.
- One of the side bottom portions 28 (side bottom portion 28 L in this preferred embodiment) is only provided integrally with a rib 28 P protruding from the bottom of the groove 28 N and extending in the vertical direction.
- the fourth seal 44 spans the grooves 28 N of both side bottom portions 28 .
- the rib 28 P of the side bottom portion 28 L is fitted in the space 44 C of the fourth seal 44 .
- the elastic portion 44 B surrounds the rib 28 P and the first protrusion 44 D in the front to back direction and is deformed in a manner following the rib 28 P and, in this state, adheres tightly to the rib 28 P.
- the second protrusion 44 F is also deformed in a manner sandwiched between the leading end of the rib 28 P and the bottom of the groove 28 N in the side bottom portion 28 R to adhere tightly to the bottom of the groove 28 N. This causes the boundary between the couplings 28 C of the pair of side bottom portions 28 to be sealed entirely in the vertical direction by the fourth seal 44 .
- the third seal 43 preferably has an annular shape extending along the annular body defined by the fitting groove 27 C in the front bottom portion 27 and the fitting grooves 28 K in the side bottom portions 28 (see FIGS. 2 and 3 ).
- the cross-section of the third seal 43 in the direction perpendicular or substantially perpendicular to the direction in which the third seal 43 extends has a structure shown in FIG. 6 at any position in the extending direction of the third seal 43 .
- the third seal 43 includes a core portion 43 A made of, for example, metal and an elastic portion 43 B made of, for example, rubber and coating the entire core portion 43 A.
- the core portion 43 A preferably has a U-shaped or substantially U-shaped cross-section and the elastic portion 43 B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to the core portion 43 A.
- the elastic portion 43 B includes a tongue-shaped first protrusion 43 D protruding into a concave space 43 C sandwiched between the core portion 43 A.
- the first protrusion 43 D is provided on one of a pair of flat regions of the inner surface of the elastic portion 43 B extending parallel or substantially parallel to each other with the space 43 C sandwiched therebetween and protrudes in a manner away from an opening 43 E of the space 43 C.
- first protrusions 43 D may be provided and, in this preferred embodiment, two first protrusions 43 D are arranged parallel or substantially parallel to each other.
- the elastic portion 43 B includes a second protrusion 43 F protruding in a direction away from the opening 43 E of the space 43 C.
- the second protrusion 43 F preferably has a circular cross-section, for example.
- the curved portion of the core portion 43 A is positioned between the space 43 C and the second protrusion 43 F.
- FIG. 7 is a schematic vertical cross-sectional rear view of the engine cover 19 in the region B of FIG. 3 .
- the third seal 43 spans the fitting groove 27 C in the front bottom portion 27 and the fitting groove 28 K in each side bottom portion 28 (the fitting groove 28 K in the side bottom portion 28 L in FIG. 7 ).
- the outer edge 18 A of the mount 18 is fitted in the space 43 C of the third seal 43 .
- the elastic portion 43 B vertically sandwiches the outer edge 18 A and the first protrusion 43 D is deformed in a manner following the outer edge 18 A and, in this state, adheres tightly to the outer edge 18 A from above.
- the second protrusion 43 F is also deformed in a manner sandwiched between the outer edge 18 A and the bottoms of the respective fitting grooves 27 C and 28 K to adhere tightly to the bottoms of these fitting grooves. This causes the boundary between the mount 18 and the front bottom portion 27 and the boundary between the mount 18 and each side bottom portion 28 to be sealed together around the entire circumference of the outer edge 18 A by the third seal 43 .
- the second seal 42 includes a second lower seal 46 and a second upper seal 47 (see FIG. 3 ).
- the second lower seal 46 preferably has an annular shape extending along the annular body defined by the upper end 27 G of the front bottom portion 27 and the upper ends 28 E of the side bottom portions 28 .
- the cross-section of the second lower seal 46 in the direction perpendicular or substantially perpendicular to the direction in which the second lower seal 46 extends has a structure shown in FIG. 8 at any position in the extending direction of the second lower seal 46 .
- the second lower seal 46 includes a core portion 46 A made of, for example, metal and an elastic portion 46 B made of, for example, rubber and coating the entire core portion 46 A.
- the core portion 46 A preferably has a vertically inverted U-shaped or substantially U-shaped cross-section and the elastic portion 46 B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to the core portion 46 A.
- the concave space 46 C sandwiched between the core portion 46 A opens downward.
- the elastic portion 46 B includes a tongue-shaped first protrusion 46 D protruding upward into the space 46 C.
- the first protrusion 46 D is provided on one of a pair of flat regions (right flat region in FIG.
- first protrusions 46 D may be provided and, in this preferred embodiment, two first protrusions 46 D are arranged parallel or substantially parallel to each other.
- the elastic portion 46 B includes, on its side surface (left side surface in FIG. 8 ), a second protrusion 46 E protruding in a direction away from the space 46 C.
- the straight portion of the core portion 46 A is positioned between the space 46 C and the second protrusion 46 E.
- the second protrusion 46 E is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from the space 46 C.
- the second upper seal 47 is made of, for example, rubber and preferably has a band shape extending along a portion of the second lower seal 46 (see FIG. 3 ).
- the cross-section of the second upper seal 47 in the direction perpendicular or substantially perpendicular to the direction in which the second upper seal 47 extends has a structure shown in FIG. 9 at any position in the extending direction of the second upper seal 47 .
- the second upper seal 47 integrally includes a fixed portion 47 A and a protrusion 47 B.
- the fixed portion 47 A preferably has a vertical plate shape.
- Adhesive 48 is provided on a side surface 47 C of the fixed portion 47 A.
- the protrusion 47 B protrudes from the side surface 47 D opposite to the side surface 47 C of the fixed portion 47 A.
- the protrusion 47 B is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from the side surfaces 47 C and 47 D.
- a pair of convex portions 47 E protruding downward are provided at lower portions of the protrusion 47 B.
- One of the convex portions 47 E protrudes in a manner coming close to the fixed portion 47 A as it extends downward, while the other convex portion 47 E protrudes in a manner away from the fixed portion 47 A as it extends downward.
- FIG. 10 is a schematic vertical cross-sectional rear view of the engine cover 19 in the region C of FIG. 3 .
- the upper end 27 G of the front bottom portion 27 and the upper ends 28 E of the side bottom portions 28 (only the upper end 28 E of the side bottom portion 28 L is shown in FIG. 10 ) are fitted in the space 46 C of the second lower seal 46 from below.
- the elastic portion 46 B laterally sandwiches the upper end 28 E and the first protrusion 46 D is deformed in a manner following the upper end 28 E and, in this state, laterally adheres tightly to the upper end 28 E (from the right in FIG. 10 ).
- the second protrusion 46 E is deformed in a manner hanging downward to adhere tightly to the lower edge 25 A of the top portion 25 from within the engine cover 19 . This causes the boundary between the top portion 25 and the front bottom portion 27 and the boundary between the top portion 25 and each side bottom portion 28 to be sealed together around the entire circumference of the lower edge 25 A by the second lower seal 46 . It is noted that the second protrusion 46 E may adhere tightly to the lower edge 25 A only laterally (see FIGS. 16 and 20 below) or may adhere tightly to the lower edge 25 A from below at the leading end 46 F of the second protrusion 46 E, as shown in FIG. 10 .
- the second upper seal 47 is located on a region rearward of the front portion of the second lower seal 46 and preferably is U-shaped or substantially U-shaped in plan view (see FIG. 3 ).
- the fixed portion 47 A of the second upper seal 47 follows the lower end of the inner surface of the top portion 25 and is applied to the top portion 25 via the adhesive 48 .
- the protrusion 47 B of the second upper seal 47 is positioned over the second lower seal 46 and adheres tightly to the second lower seal 46 with the pair of convex portions 47 E sandwiching an upper portion of the second lower seal 46 .
- a pair of left and right first seals 41 are provided correspondingly to the pair of left and right side bottom portions 28 (see FIG. 3 ).
- the left first seal 41 will be referred to as a first seal 41 L
- the right first seal 41 will be referred to as a first seal 41 R.
- the first seal 41 L and the first seal 41 R are preferably laterally symmetric. While the first seals 41 will hereinafter be described focusing on the first seal 41 L, the following description of the first seal 41 L, when reversed laterally, corresponds to description of the first seal 41 R.
- FIG. 11 is a schematic perspective view of the first seal 41 L.
- the first seal 41 L integrally includes a first portion 51 exemplifying a three-part seal, a second portion 52 , and a third portion 53 exemplifying a two-part seal.
- the first portion 51 is arranged at a position higher than that of the second portion 52 and the third portion 53 extends from the first portion 51 to the second portion 52 .
- the first portion 51 and the second portion 52 are, for example, rubber molded articles and the third portion 53 is a rubber extrusion molded article inserted in the molded articles.
- the joint between the first portion 51 and the third portion 53 and the joint between the second portion 52 and the third portion 53 are respectively indicated by alternate long and short dashed lines.
- the first portion 51 , the second portion 52 , and the third portion 53 are preferably made of the same rubber material.
- the first portion 51 , the second portion 52 , and the third portion 53 will hereinafter be described in this order.
- the first portion 51 integrally includes an inner portion 51 A and an outer portion 51 B.
- the inner portion 51 A preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the lateral direction.
- the upper edge and the rear edge of the inner portion 51 A are bent rightward.
- a pair of anteroposterior vertical ribs 51 C protruding leftward and extending vertically and parallel or substantially parallel to each other are provided in a front end of the left surface of the inner portion 51 A.
- the forward vertical rib 51 C may be referred to as a vertical rib 51 CF
- the rearward vertical rib 51 C may be referred to as a vertical rib 51 CR.
- the vertical rib 51 CF defines a front edge of the inner portion 51 A bent leftward.
- a vertically extending water storage groove 51 D is located between and defined by the two vertical ribs 51 C.
- An upper rib 51 E protruding leftward is provided at a position of the left surface of the inner portion 51 A below and adjacent to the upper edge.
- the upper rib 51 E is connected to the upper end of the vertical rib 51 CF to close the upper end of the water storage groove 51 D and extends rearward from the upper end of the water storage groove 51 D to just before the rear edge of the inner portion 51 A.
- a rear end of the upper rib 51 E may be curved downward.
- a guide 51 F is provided in a lower end of the left surface of the inner portion 51 A.
- the guide 51 F is a leftward protruding rib connected to a lower end of the vertical rib 51 CF to close the lower end of the water storage groove 51 D and extends rearward from the lower end of the water storage groove 51 D to just before the rear edge of the inner portion 51 A.
- An insertion hole 51 G laterally penetrates a portion of the inner portion 51 A that is rearward of the water storage groove 51 D and is vertically sandwiched between the upper rib 51 E and the guide 51 F.
- the inner portion 51 A further includes an extended portion 51 H extending leftward from the left end of the guide 51 F and a lower rib 51 I protruding leftward and upward from the boundary between the guide 51 F and the extended portion 51 H.
- the extended portion 51 H is connected to the lower end of the vertical rib 51 CF and extends rearward behind the guide 51 F.
- a rear portion 51 J of the extended portion 51 H is curved downward.
- a left end of the rear portion 51 J is bent downward.
- the lower rib 51 I is connected to the lower end of the vertical rib 51 CF and extends along the extended portion 51 H.
- a drainage groove 51 K is located between and defined by the extended portion 51 H and the lower rib 51 I. The drainage groove 51 K extends rearward from the lower end of the vertical rib 51 CF to be curved downward and opens leftward.
- the outer portion 51 B preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the lateral direction and inclined with respect to the inner portion 51 A in plan view so as to be offset rightward as it extends forward.
- An upper end 51 L of the outer portion 51 B protrudes upward above the inner portion 51 A.
- the upper end edge of the outer portion 51 B is inclined so as to be offset downward as it extends forward.
- the rear edge 51 M of the outer portion 51 B is bent rightward. An upper end of the rear edge 51 M defines a portion of the upper end 51 L.
- the upper end of the rear edge 51 M protrudes upward above the vertical rib 51 CF of the inner portion 51 A, and a portion of the rear edge 51 M lower than the upper end is connected to the vertical rib 51 CF from the left.
- the lower edge 51 N of the outer portion 51 B is bent leftward.
- a rear end of the lower edge 51 N is bent downward and connected to the lower end of the vertical rib 51 CF from the left.
- the rear edge 51 M and the rear end of the lower edge 51 N may be considered to be a portion of the vertical rib 51 CF or the vertical rib 51 CF may be considered to be a portion of the rear edge 51 M and the lower edge 51 N.
- the water storage groove 51 D in the inner portion 51 A is adjacent to the rear edge 51 M from behind.
- the second portion 52 preferably has a box shape and its interior space opens downward.
- the second portion 52 preferably has a triangular or substantially triangular top surface 52 A, and a front surface 52 B, a sealing surface 52 C, and a tapered surface 52 D extending downward from the three respective sides of the top surface 52 A.
- the second portion 52 also includes a pressed surface 52 E sandwiched between the sealing surface 52 C and the tapered surface 52 D.
- the top surface 52 A extends horizontally or substantially horizontally.
- the front surface 52 B extends in or substantially in the lateral direction.
- a vertically extending positioning groove 52 F is provided at a lateral intermediate position of the front surface 52 B.
- the positioning groove 52 F penetrates vertically through the second portion 52 .
- a protrusion 52 G defining the upper end of the positioning groove 52 F and protruding upward is provided on the top surface 52 A.
- the horizontal cross-section of the protrusion 52 G preferably is U-shaped or substantially U-shaped narrowing rearward.
- a rear end of the protrusion 52 G is the leading end of the protrusion 52 G and is preferably hollow.
- the interior space in the leading end of the protrusion 52 G defines an outlet 52 H (see FIG. 17 below) opening downward from the interior space of the second portion 52 .
- a projection 52 I protruding upward is provided on the top surface 52 A.
- the projection 52 I extends rearward from the leading end of the protrusion 52 G to be bent leftward.
- the sealing surface 52 C is connected to the right end edge of the front surface 52 B and inclined so as to offset rearward as it extends leftward in plan view.
- the sealing surface 52 C may be flat or curved in a manner recessed forward in plan view.
- the tapered surface 52 D is connected to the left end edge of the front surface 52 B and inclined so as to offset downward as it extends leftward.
- the rear end of the upper end edge of the tapered surface 52 D is connected to the left end of the upper end edge of the sealing surface 52 C.
- a lower end of the tapered surface 52 D may be a vertical surface.
- the left end of the projection 52 I is positioned at approximately the center of the upper end edge of the tapered surface 52 D.
- the pressed surface 52 E is bridged between the left end edge of the sealing surface 52 C and the rear end edge of the tapered surface 52 D and preferably has a triangular or substantially triangular shape widening downward.
- the pressed surface 52 E is inclined so as to offset forward as it extends leftward in plan view.
- the third portion 53 preferably has a columnar shape extending front to back between the first portion 51 and the second portion 52 in a manner inclined with respect to the horizontal direction.
- the cross-section of the third portion 53 in the direction perpendicular or substantially perpendicular to the direction in which the third portion 53 extends has a structure shown in FIG. 12 at any position in the extending direction of the third portion 53 .
- the thus simply shaped third portion 53 having the same cross-section at any position is different in structure from the first portion 51 and the second portion 52 having their respective complex shapes.
- the third portion 53 includes a core portion 53 A made of, for example, metal and an elastic portion 53 B made of, for example, rubber and coating the entire core portion 53 A.
- the core portion 53 A preferably has a vertically inverted U-shaped or substantially U-shaped cross-section and the elastic portion 53 B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to the core portion 53 A.
- the concave space 53 C sandwiched between the core portion 53 A opens downward.
- a front end of the elastic portion 53 B is connected to the rear portion 51 J of the extended portion 51 H and the lower rib 51 I of the first portion 51 , while a rear end of the elastic portion 53 B is connected to the protrusion 52 G of the second portion 52 (see FIG. 11 ).
- the elastic portion 53 B includes a tongue-shaped first protrusion 53 D protruding leftward and upward in the space 53 C.
- the first protrusion 53 D is provided on one of a pair of left and right flat regions (right flat region in FIG. 12 ) of the inner surface of the elastic portion 53 B extending parallel or substantially parallel to each other with the space 53 C sandwiched therebetween.
- Multiple first protrusions 53 D may be provided and, in this preferred embodiment, two first protrusions 53 D are arranged parallel or substantially parallel to each other.
- a concavo-convex portion 53 F defined by alternating concaves and convexes is provided vertically on the other one 53 E of the pair of left and right flat regions (left flat region in FIG. 12 ) of the inner surface of the elastic portion 53 B.
- the elastic portion 53 B includes a second protrusion 53 G protruding upward from an upper end of the core portion 53 A.
- the second protrusion 53 G is hollow and preferably has a triangular or substantially triangular cross-section narrowing upward.
- the interior space of the second protrusion 53 G defines a flow path 53 H connected to the drainage groove 51 K in the first portion 51 (see FIG. 11 ) and the outlet 52 H of the second portion 52 (see FIG. 17 ).
- FIG. 13 is a schematic left side view of the first seal 41 L and its periphery.
- the front bottom portion 27 and the second lower seal 46 are shown as the periphery.
- the first seal 41 L is arranged along the left opposing portion 27 H in the upper end 27 G of the front bottom portion 27 and the upper end edge of the left rear portion 27 J of the vertical portion 27 B.
- the first portion 51 , the second portion 52 , and the third portion 53 of the first seal 41 L in this state will hereinafter be described in this order.
- FIG. 14 is an end view of a cut portion along the line A-A in FIG. 13 .
- At least a portion of the inner portion 51 A of the first portion 51 is located between the left opposing portion 27 H in the front bottom portion 27 and the bottom portion 28 G of the recess 28 F in the upper end 28 E of the side bottom portion 28 L.
- a raised portion 27 K raised outward (leftward in FIG. 14 ) in a manner encompassing the screw hole 27 I is provided on the outer surface (left surface in FIG. 14 ) of the opposing portion 27 H.
- the raised portion 27 K is fitted in the insertion hole 51 G in the first portion 51 with no clearance gap.
- a screw portion 29 A of the coupling member 29 that couples the opposing portion 27 H and the side bottom portion 28 L is assembled into the screw hole 27 I while being inserted through the insertion hole 51 G.
- a cylindrical collar 60 encompassing the screw portion 29 A and a cylindrical grommet 61 fitted in the insertion hole 28 H in the bottom portion 28 G while encompassing the collar 60 .
- the collar 60 is preferably made of metal, while the grommet 61 is preferably made of resin.
- a peripheral portion of the insertion hole 28 H in the side bottom portion 28 L is fitted entirely with no clearance gap in a fitting groove 61 A provided in the outer peripheral surface of the grommet 61 .
- the upper edge of the inner portion 51 A is engaged with the opposing portion 27 H from above, while the rear edge of the inner portion 51 A is engaged with the opposing portion 27 H from behind.
- the vertical rib 51 CR, the upper rib 51 E, and the lower rib 51 I protrude toward the upper end 28 E of the side bottom portion 28 L and adhere tightly to the inner surface of the side bottom portion 28 L.
- the vertical rib 51 CR and the upper rib 51 E extend leftward to adhere tightly to the right surface of the bottom portion 28 G in the upper end 28 E, while the lower rib 51 I is deformed in a manner following the lower surface of the bottom portion 28 G to adhere tightly to the lower surface of the bottom portion 28 G.
- the clearance gap 62 between the opposing portion 27 H and the bottom portion 28 G is closed by the vertical rib 51 CR from the front and also closed by the upper rib 51 E and the lower rib 51 I from above and below to be opened only rearward.
- the water storage groove 51 D in the inner portion 51 A which is positioned forward of the vertical rib 51 CR, is opposed to the upper end 28 E of the side bottom portion 28 L (particularly a region of the right surface of the bottom portion 28 G forward of the insertion hole 28 H).
- FIG. 15 is a schematic perspective view of the first portion 51 and its periphery.
- the front bottom portion 27 and the side bottom portion 28 L are shown as the periphery.
- the outer portion 51 B of the first portion 51 is arranged on the outer surface of the upper end 27 G of the front bottom portion 27
- the rear edge 51 M of the outer portion 51 B closes the boundary between the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surface of the upper end 28 E of the side bottom portion 28 L. That is, the outer portion 51 B is arranged on the outer surface of the upper end 27 G of the front bottom portion 27 through the boundary.
- the lower edge 51 N of the outer portion 51 B is arranged along a left rear end of the horizontal step 27 E and an upper end of the left vertical step 27 F.
- FIG. 16 is an end view of a cut portion along the line B-B in FIG. 13 .
- the boundary between the top portion 25 and the front bottom portion 27 and the boundary between the top portion 25 and each side bottom portion 28 are sealed together by the second lower seal 46 .
- the elastic portion 46 B of the second lower seal 46 sandwiching the upper end 27 G of the front bottom portion 27 sandwiches the upper end 51 L, which is a portion of the outer portion 51 B, between the same and the outer surface of the upper end 27 G.
- the first boundary B 1 between the top portion 25 , the front bottom portion 27 , and the side bottom portion 28 L is sealed by both the first portion 51 and the second lower seal 46 .
- FIG. 17 is a cross-sectional view taken along the line C-C in FIG. 13 .
- FIG. 18 is an end view of a cut portion along the line D-D in FIG. 13 .
- FIG. 19 is a cross-sectional view taken along the line E-E in FIG. 18 .
- a right portion of the second portion 52 is housed in a left end of the fitting groove 27 C in the front bottom portion 27 (see also FIG. 2 ).
- the sealing surface 52 C of the second portion 52 is smoothly continuous with a region (not shown) of the bottom of the fitting groove 27 C adjoining the second portion 52 from the right.
- the sealing surface 52 C of the second portion 52 in this state adheres tightly to the second protrusion 43 F of the third seal 43 from the front and left at the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portion 28 L.
- the positioning groove 52 F and a portion of the second portion 52 to the left of the positioning groove 52 F stick out leftward from the fitting groove 27 C.
- a rear end of the left rear portion 27 J in the vertical portion 27 B of the front bottom portion 27 will be referred to as a positioning portion 27 L.
- the positioning portion 27 L is fitted in the positioning groove 52 F from the front (see FIG. 17 ).
- a pair of upper and lower horizontal walls 27 M extending rearward parallel or substantially parallel to each other and a vertical wall 27 N extending upward from the front end of the lower horizontal wall 27 M are provided on the rear edge of the horizontal portion 27 A of the front bottom portion (see FIG. 19 ).
- the fitting groove 27 C in the front bottom portion 27 defines a space between the pair of horizontal walls 27 M and the vertical wall 27 N defines the bottom of the fitting groove 27 C.
- the second portion 52 which is partially housed in the fitting groove 27 C, is sandwiched vertically between the pair of horizontal walls 27 M and in contact with the vertical wall 27 N from behind. This causes the second portion 52 to be positioned vertically and anteroposteriorly.
- the projection 52 I on the top surface 52 A of the second portion 52 adheres tightly to the upper horizontal wall 27 M.
- the front region of the fitting groove 28 K in each side bottom portion 28 is deeper than the rear region (see the fitting groove 28 K in the side bottom portion 28 R in FIG. 2 ).
- the engine cover 19 further includes a raised portion 63 to be attached to each side bottom portion 28 (see FIG. 17 ).
- the raised portion 63 is, for example, a hollow body, which is housed in the front region of the fitting groove 28 K to raise the front region of the fitting groove 28 K. This fills the gap between the outer surface 28 Q of the side bottom portion 28 defining a design surface and the outer edge 18 A of the mount 18 .
- the raised portion 63 includes a sealing surface 63 A continuous with the sealing surface 52 C of the second portion 52 and the bottom (not shown) of the rear region of the fitting groove 28 K, and a pressing surface 63 B bent from the front end of the sealing surface 63 A to extend laterally outward (leftward in the case of the side bottom portion 28 L) in an inclined manner.
- the sealing surface 63 A adheres tightly to the second protrusion 43 F of the third seal 43 from the left.
- the pressing surface 63 B presses against the pressed surface 52 E of the second portion 52 from the left and behind.
- the upper rib 28 I and the lower rib 28 J vertically sandwiching the fitting groove 28 K in each side bottom portion 28 , the upper rib 28 I protrudes inside the engine cover 19 farther inward than the lower rib 28 J to be placed on the top surface 52 A of the second portion 52 (see FIG. 18 ).
- the side bottom portion 28 L is attached to the front bottom portion 27 from the left.
- the upper rib 28 I of the side bottom portion 28 L is guided by the tapered surface 52 D of the second portion 52 to be placed smoothly on the top surface 52 A.
- the projection 52 I on the top surface 52 A adheres tightly not only to the upper horizontal wall 27 M of the fitting groove 27 C in the front bottom portion 27 as mentioned above, but also to the upper rib 28 I (see FIGS. 18 and 19 ). This causes the clearance gap between the fitting groove 27 C and the fitting groove 28 K to be closed by the projection 52 I.
- the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portion 28 L is sealed by both the second portion 52 and the third seal 43 .
- the upper horizontal wall 27 M is provided with a vertical wall 27 R (see also FIG. 2 ) with its thickness direction coinciding or substantially coinciding with the lateral direction, and the vertical wall 27 R adjoins the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portion 28 L from the right. This allows the vertical wall 27 R to prevent external water from entering into the engine cover 19 through the boundary as a sheet of spray.
- FIG. 20 is an end view of a cut portion along the line F-F in FIG. 13 .
- the first seal 41 L the upper end of the left rear portion 27 J of the front bottom portion 27 is fitted in the space 53 C in the third portion 53 from below.
- the elastic portion 53 B laterally sandwiches the upper end of the rear portion 27 J and the first protrusion 53 D is deformed in a manner following the upper end of the rear portion 27 J and, in this state, laterally adheres tightly to the rear portion 27 J (from the right in FIG. 20 ).
- the concavo-convex portion 53 F see also FIG.
- the elastic portion 53 B which is positioned opposite to the first protrusion 53 D with respect to the rear portion 27 J, is also compressed between the upper end of the rear portion 27 J and the core portion 53 A to adhere tightly to the rear portion 27 J.
- the second protrusion 53 G of the third portion 53 is deformed in a manner sandwiched between the rear portion 27 J and the extended section 28 M of the side bottom portion 28 L to adhere tightly to the extended section 28 M from below. This causes the second boundary B 2 between the front bottom portion 27 and the side bottom portion 28 L to be sealed by the third portion 53 entirely in the front to back direction.
- the leading end 53 I of the second protrusion 53 G is continuous with the lower rib 51 I of the first portion 51 and the projection 52 I of the second portion 52 .
- the first seal 41 is therefore provided with a single seal line 54 defined by the upper rib 51 E, the vertical rib 51 CR, and the lower rib 51 I of the first portion 51 , the projection 52 I of the second portion 52 , and the leading end 53 I of the third portion 53 (see FIG. 11 ).
- the boundary between the front bottom portion 27 and the side bottom portion 28 L is sealed along the seal line 54 .
- the engine cover 19 is divisible into three or more divided covers including the top portion 25 , the front bottom portion 27 , and the side bottom portions 28 (see FIG. 2 ).
- the engine cover 19 thus includes the boundary (first boundary B 1 ) between the top portion 25 , the front bottom portion 27 , and the side bottom portions 28 and the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portions 28 .
- the first seal 41 L of the sealing structure 40 seals the boundary (first boundary B 1 ) between the top portion 25 , the front bottom portion 27 , and the side bottom portion 28 L with the first portion 51 (see FIGS. 14 to 16 ).
- the first seal 41 L seals the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portion 28 L with the second portion 52 (see FIGS. 17 to 19 ).
- the first seal 41 L seals the other boundary (the second boundary B 2 between the front bottom portion 27 and the side bottom portion 28 L) extending between these boundaries with the third portion 53 (see FIG. 20 ).
- the first seal 41 R of the sealing structure 40 seals the boundary (first boundary B 1 ) between the top portion 25 , the front bottom portion 27 , and the side bottom portion 28 R with the first portion 51 and seals the boundary between the front bottom portion 27 , the mount 18 , and the side bottom portion 28 R with the second portion 52 .
- the first seal 41 R seals the other boundary (the second boundary B 2 between the front bottom portion 27 and the side bottom portion 28 R) extending between these boundaries with the third portion 53 .
- the second seal 42 of the sealing structure 40 provides desirable sealing characteristics at the boundary between the top portion 25 and the front bottom portion 27 and the boundary between the top portion 25 and each side bottom portion 28 (see FIG. 10 ).
- the third seal 43 of the sealing structure 40 provides desirable sealing characteristics at the boundary between the mount 18 and the front bottom portion 27 and the boundary between the mount 18 and each side bottom portion 28 (see FIG. 7 ).
- the fourth seal 44 of the sealing structure 40 seals the boundary between the pair of side bottom portions 28 (see FIG. 5 ).
- the first portion 51 seals the clearance gap 62 between the opposing portion 27 H in the upper end 27 G of the front bottom portion 27 and the upper end 28 E of each side bottom portion 28 with the inner portion 51 A (see FIG. 14 ). Further, the first portion 51 seals the boundary between the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surface of the upper end 28 E of each side bottom portion 28 with the rear edge 51 M of the outer portion 51 B (see FIG. 15 ). This provides desirable sealing characteristics at the boundary between the upper end 27 G of the front bottom portion 27 and the upper end 28 E of each side bottom portion 28 . This significantly reduces or prevents external water from leaking through the boundary between the upper end 28 E of each side bottom portion 28 and the upper end 27 G of the front bottom portion 27 and entering into the engine 13 .
- the inner portion 51 A is arranged in a manner offset by one step inside the engine cover 19 farther inward than the outer portion 51 B, external water is less likely to reach the inner portion 51 A through the boundary between the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surface of the upper end 28 E of the side bottom portion 28 . Even if external water leaks through the boundary between the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surface of the upper end 28 E of each side bottom portion 28 and enters into the engine cover 19 , the water is immediately contained in the water storage groove 51 D in the inner portion 51 A. It is therefore difficult for the water to reach the engine 13 . This further significantly reduces or prevents water from entering into the engine 13 .
- the interior of the engine cover 19 has a negative pressure due to the air-intake by the engine 13 .
- Water within the water storage groove 51 D therefore tends to scatter toward the air-intake structure (not shown) upward and taken into the engine 13 .
- the water within the water storage groove 51 D is blocked by the upper rib 51 E from scattering upward within the engine cover 19 to reach the engine 13 , which further significantly reduces or prevents water from entering into the engine 13 .
- Water within the water storage groove 51 D slides on the guide 51 F (see FIG. 11 ) to be guided rearward by the guide 51 F. This causes the water to fall out of the guide 51 F to be guided into the drainage hole 27 D in the engine cover 19 and/or the drainage hole 18 D in the mount 18 (see FIG. 2 ) and eventually discharged out of the engine cover 19 , which further significantly reduces or prevents water from entering into the engine 13 .
- External water may reach not the water storage groove 51 D or the insertion hole 51 G but the drainage groove 51 K (see FIG. 11 ) within the inner portion 51 A.
- water within the drainage groove 51 K flows through the flow path 53 H within the second protrusion 53 G of the third portion 53 (see FIG. 20 ) to flow down through the outlet 52 H of the second portion 52 (see FIG. 17 ) downward from the second portion 52 to be discharged through the drainage hole 27 D in the engine cover 19 and/or the drainage hole 18 D in the mount 18 .
- the second seal 42 sandwiches the upper end 51 L of the outer portion 51 B, which seals the boundary between the outer surface of the upper end 27 G of the front bottom portion 27 and the outer surface of the upper end 28 E of each side bottom portion 28 in the first seal 41 , between the same and the front bottom portion 27 (see FIG. 16 ).
- This causes the first seal 41 and the second seal 42 to be continuous with each other. Since the boundary (first boundary B 1 ) between the top portion 25 , the front bottom portion 27 , and each side bottom portion 28 is thus sealed by both the first seal 41 and the second seal 42 , desirable sealing characteristics are provided at the boundary. This significantly reduces or prevents external water from leaking through the boundary and entering into the engine 13 .
- the sealing surface 52 C of the second portion 52 adheres tightly to the third seal 43 from the front at the boundary between the front bottom portion 27 , the mount 18 , and each side bottom portion 28 to seal the boundary (see FIG. 17 ).
- the second portion 52 may be positioned laterally by the positioning groove 52 F and the positioning portion 27 L to seal the boundary between the front bottom portion 27 , the mount 18 , and each side bottom portion 28 with the lateral position being stabilized. This provides desirable sealing characteristics at the boundary and thus significantly reduces or prevents external water from leaking through the boundary and entering into the engine 13 .
- the first portion 51 and the second portion 52 are preferably molded articles, while the third portion 53 is preferably an extrusion molded article, which makes it possible to achieve the structure in which the first seal 41 integrally includes the first portion 51 , the second portion 52 , and the third portion 53 .
- the clearance gap at the complex first boundary B 1 spanning the three portions of the top portion 25 , the front bottom portion 27 , and each side bottom portion 28 is filled with the first portion 51 , which is a molded article.
- the clearance gap at the complex boundary spanning the three portions of the front bottom portion 27 , the mount 18 , and each side bottom portion 28 is filled with the second portion 52 , which is also a molded article.
- the clearance gap at the relatively simple second boundary B 2 spanning the two portions of the front bottom portion 27 and each side bottom portion 28 is filled with the third portion 53 , which is an extrusion molded article. This allows the first seal 41 to seal together the boundaries.
- only one of the pair of side bottom portions 28 may be provided separately and the other side bottom portion 28 may be integral with the top portion 25 or the front bottom portion 27 .
- only one first seal 31 may also be provided correspondingly to the separate side bottom portion 28 .
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Abstract
Description
- This application claims the benefit of priority to Japanese Patent Application No. 2017-095809 filed on May 12, 2017. The entire contents of this application are hereby incorporated herein by reference.
- The present invention relates to an outboard motor and a sealing structure for a divisible engine cover used therefor.
- The outboard motor described in Japanese Unexamined Patent Application Publication No. H6-234393 includes a motor cowl covering an engine, the motor cowl being divisible into an upper motor cover and a lower motor cover. The boundary between the lower end of the upper motor cover and the upper end of the lower motor cover is sealed with a cover seal that is annular in plan view. The lower motor cover is divisible into a first cover portion and a second cover portion.
- The motor cowl described in Japanese Unexamined Patent Application Publication No. H6-234393 has a boundary spanning three parts of the upper motor cover, the first cover portion, and the second cover portion and another boundary continuous with the boundary and existing between the two parts of the first cover portion and the second cover portion. With just the annular, i.e., simply shaped, cover seal disclosed in Japanese Unexamined Patent Application Publication No. H6-234393, it is difficult to seal these boundaries without leakage, and external water may leak through the boundaries and enter into the engine cover. When the water within the engine cover enters into the engine, a problem may occur with the engine.
- In order to overcome the previously unrecognized and unsolved challenges described above, a preferred embodiment of the present invention provides an outboard motor including an engine, an engine cover including at least a first cover, a second cover, and a third cover that cover the engine, and a seal. The engine cover includes a first boundary spanning three portions of the first cover, the second cover, and the third cover and a second boundary between two of the three portions and continuous with the first boundary. The seal integrally includes a three-part seal that seals the first boundary and a two-part seal with a structure different from that of the three-part seal and that seals the second boundary.
- In accordance with the preferred embodiment described above, the engine cover is divisible into at least the first cover, the second cover, and the third cover, has the first boundary spanning three portions of the three covers and the second boundary between two of the three portions and continuous with the first boundary. The seal integrally includes the three-part seal and the two-part seal, which seal the first boundary and the second boundary and have respective different structures. The seal seals the first boundary and the second boundary with the three-part seal sealing the first boundary and the two-part seal sealing the second boundary. This significantly reduces or prevents external water from leaking through the first boundary and the second boundary, which are boundaries between the covers of the divisible engine cover, and entering into the engine.
- In a preferred embodiment of the present invention, the three-part seal may be a molded article and the two-part seal may be an extrusion molded article.
- In accordance with the preferred embodiment described above, a clearance gap in the complex shaped first boundary spanning the three portions is filled with the molded three-part seal and a clearance gap in the second boundary spanning the two portions is filled with the extrusion molded two-part seal. This allows the seal to seal the first boundary and the second boundary.
- A preferred embodiment of the present invention provides an outboard motor including an engine, a mount on which the engine is mounted, an engine cover, and a sealing structure for the engine cover. The engine cover includes a top portion opposing the engine from above, a front bottom portion opposing the engine from the front, and a side bottom portion opposing the engine from the side. The front bottom portion is located at a position lower than a position of the top portion, and the side bottom portion is located at a position lower than the position of the top portion and rearward of the front bottom portion. The engine cover is coupled to the mount through the front bottom portion and the side bottom portion. The sealing structure includes a first seal. The first seal integrally includes a first portion, a second portion, and a third portion extending from the first portion to the second portion. The first portion seals the boundary between the top portion, the front bottom portion, and the side bottom portion. The second portion seals the boundary between the front bottom portion, the mount, and the side bottom portion. The third portion seals the boundary between the front bottom portion and the side bottom portion.
- In accordance with the preferred embodiment described above, an engine cover, which is divisible into three or more covers including at least the top portion, the front bottom portion, and the side bottom portion, includes a boundary between the top portion, the front bottom portion, and the side bottom portion and a boundary between the front bottom portion, the mount, and the side bottom portion. The first seal of the sealing structure seals the boundary between the top portion, the front bottom portion, and the side bottom portion with the first portion; seals the boundary between the front bottom portion, the mount, and the side bottom portion with the second portion; and seals the other boundary extending between these boundaries with the third portion. This structure provides desirable sealing characteristics for a divisible engine cover having such a complex structure. This significantly reduces or prevents external water from leaking through the boundaries between the multiple covers of the divisible engine cover and entering into the engine.
- In a preferred embodiment of the present invention, the first portion may be located at a position higher than a position of the second portion, and an upper end of the front bottom portion may include an opposing portion that opposes an upper end of the side bottom portion from within the engine cover. In this case, the first portion integrally includes an inner portion and an outer portion. The inner portion is at least partially located between the opposing portion and the upper end of the side bottom portion. The outer portion extends through the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion so as to be located on the outer surface of the upper end of the front bottom portion. The inner portion includes a water storage groove adjacent to the outer portion and opposing the side bottom portion.
- In accordance with the preferred embodiment described above, the first portion seals the boundary between the opposing portion in the upper end of the front bottom portion and the upper end of the side bottom portion with the inner portion and seals the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion with the outer portion. This structure provides desirable sealing characteristics at the boundary between the upper end of the front bottom portion and the upper end of the side bottom portion. This significantly reduces or prevents external water from leaking through the boundary between the upper end of the side bottom portion and the upper end of the front bottom portion and entering into the engine.
- Even if external water leaks through the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion and enters into the engine cover, the water is immediately contained in the water storage groove in the inner portion so that it is difficult to reach the engine. This further significantly reduces or prevents water from entering into the engine.
- In a preferred embodiment of the present invention, the inner portion may include an upper rib protruding toward the upper end of the side bottom portion and extending rearward from the upper end of the water storage groove.
- In accordance with the preferred embodiment described above, water within the water storage groove will be blocked by the upper rib from scattering upward within the engine cover to reach the engine, which further significantly reduces or prevents water from entering into the engine.
- In a preferred embodiment of the present invention, a drainage hole may be provided in a lower portion of the engine cover or the mount, and the inner portion may include a guide extending rearward from the lower end of the water storage groove to guide water within the water storage groove to the drainage hole.
- In accordance with the preferred embodiment described above, water within the water storage groove is guided through the guide to the drainage hole and discharged out of the engine cover, which further significantly reduces or prevents water from entering into the engine.
- In a preferred embodiment of the present invention, an insertion hole, through which a fastening member coupling the opposing portion and the side bottom portion is inserted, may be provided in a penetrating manner in a portion of the inner portion located between the upper rib and the guide.
- In accordance with the preferred embodiment described above, even if external water reaches the insertion hole, the water is blocked by the upper rib from scattering upward to reach the engine and also is guided through the guide to the drainage hole to be discharged out of the engine cover. This further significantly reduces or prevents water from entering into the engine.
- In a preferred embodiment of the present invention, the sealing structure may further include a second seal that seals the boundary between the top portion and the front bottom portion and the boundary between the top portion and the side bottom portion. In this case, the second seal may surround a portion of the outer portion located between the second seal and the front bottom portion.
- In accordance with the preferred embodiment described above, the second seal provides desirable sealing characteristics at the boundary between the top portion and the front bottom portion and the boundary between the top portion and the side bottom portion. This significantly reduces or prevents external water from leaking through these boundaries and entering into the engine.
- Further, the second seal surrounds a portion of the outer portion, which seals the boundary between the outer surface of the upper end of the front bottom portion and the outer surface of the upper end of the side bottom portion in the first seal, between the second seal and the front bottom portion. This causes the first seal and the second seal to be continuous with each other. Since the boundary between the top portion, the front bottom portion, and the side bottom portion is thus sealed by both the first seal and the second seal, this structure provides desirable sealing characteristics at the boundary. This significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- In a preferred embodiment of the present invention, the sealing structure may further include a third seal that seals the boundary between the mount and the front bottom portion and the boundary between the mount and the side bottom portion. In this case, the second portion includes a sealing surface that adheres to the third seal from the front at the boundary between the front bottom portion, the mount, and the side bottom portion.
- In accordance with the preferred embodiment described above, the third seal provides desirable sealing characteristics at the boundary between the mount and the front bottom portion and the boundary between the mount and the side bottom portion. This significantly reduces or prevents external water from leaking through these boundaries and entering into the engine.
- Further, in the first seal, the sealing surface of the second portion adheres tightly to the third seal from the front at the boundary between the front bottom portion, the mount, and the side bottom portion to seal the boundary. This causes the first seal and the third seal to be continuous with each other. Since the boundary is thus sealed by both the first seal and the third seal, desirable sealing characteristics at the boundary are achieved. This significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- In a preferred embodiment of the present invention, a longitudinally extending positioning groove may be provided in the second portion, and the front bottom portion may include a positioning portion fitted into the positioning groove.
- In accordance with the preferred embodiment described above, the second portion is preferably positioned laterally to seal the boundary between the front bottom portion, the mount, and the side bottom portion with the lateral position being stabilized. This structure provides desirable sealing characteristics at the boundary and significantly reduces or prevents external water from leaking through the boundary and entering into the engine.
- In a preferred embodiment of the present invention, the first portion and the second portion may be molded articles and the third portion may be an extrusion molded article.
- In accordance with the preferred embodiment described above, it is possible to achieve a structure in which the first seal integrally includes the first portion, the second portion, and the third portion.
- In a preferred embodiment of the present invention, the engine cover may be divisible into the top portion, the front bottom portion, and a pair of the left and right side bottom portions opposing the engine, respectively, from the left and the right. In this case, the sealing structure includes a pair of the left and right first seals. The sealing structure may further include a fourth seal that seals the boundary between the pair of side bottom portions.
- In accordance with the preferred embodiment described above, the divisible engine cover has a more complex structure due to it being divided into four or more covers of the top portion, the front bottom portion, and the pair of left and right side bottom portions. The pair of left and right first seals correspond to the pair of left and right side bottom portions.
- The left first seal seals the boundary between the top portion, the front bottom portion, and the left side bottom portion with the first portion and seals the boundary between the front bottom portion, the mount, and the left side bottom portion with the second portion. The left first seal seals the other boundary extending between these boundaries with the third portion.
- The right first seal seals the boundary between the top portion, the front bottom portion, and the right side bottom portion with the first portion and seals the boundary between the front bottom portion, the mount, and the right side bottom portion with the second portion. The right first seal seals the other boundary extending between these boundaries with the third portion.
- Further, the fourth seal seals the boundary between the pair of side bottom portions.
- As described heretofore, it is possible to provide desirable sealing characteristics for a divisible engine cover having such a complex structure. This significantly reduces or prevents external water from leaking through the boundaries between the multiple covers of the divisible engine cover and entering into the engine.
- The above and other elements, features, steps, characteristics and advantages of the present invention will become more apparent from the following detailed description of the preferred embodiments with reference to the attached drawings.
-
FIG. 1 is a schematic perspective view of an outboard motor according to a preferred embodiment of the present invention. -
FIG. 2 is a schematic exploded perspective view of an upper portion of an outboard motor main body in the outboard motor. -
FIG. 3 is a perspective view of a sealing structure for a divisible engine cover in the outboard motor main body. -
FIG. 4 is a schematic cross-sectional view showing a natural state prior to deformation of a fourth seal in the sealing structure. -
FIG. 5 is a schematic horizontal cross-sectional view of the engine cover in the region A ofFIG. 3 . -
FIG. 6 is a schematic cross-sectional view showing a natural state prior to deformation of a third seal in the sealing structure. -
FIG. 7 is a schematic vertical cross-sectional view of the engine cover in the region B ofFIG. 3 . -
FIG. 8 is a schematic cross-sectional view showing a natural state prior to deformation of a second lower seal in the sealing structure. -
FIG. 9 is a schematic cross-sectional view showing a natural state prior to deformation of a second upper seal in the sealing structure. -
FIG. 10 is a schematic vertical cross-sectional view of the engine cover in the region C ofFIG. 3 . -
FIG. 11 is a schematic perspective view of a first seal in the sealing structure. -
FIG. 12 is a schematic cross-sectional view showing a natural state prior to deformation of a third portion in the first seal. -
FIG. 13 is a schematic left side view of the first seal and its periphery. -
FIG. 14 is an end view of a cut portion along the line A-A inFIG. 13 . -
FIG. 15 is a schematic perspective view of the first portion of the first seal and its periphery. -
FIG. 16 is an end view of a cut portion along the line B-B inFIG. 13 . -
FIG. 17 is a cross-sectional view taken along the line C-C inFIG. 13 . -
FIG. 18 is an end view of a cut portion along the line D-D inFIG. 13 . -
FIG. 19 is a cross-sectional view taken along the line E-E inFIG. 18 . -
FIG. 20 is an end view of a cut portion along the line F-F inFIG. 13 . - Preferred embodiments of the present invention will hereinafter be described in detail with reference to the accompanying drawings.
FIG. 1 is a schematic front perspective view of anoutboard motor 1 according to a preferred embodiment of the present invention. Theoutboard motor 1 shown inFIG. 1 is in a basic posture. In the basic posture, therotation axis 2A of apropeller 2 in theoutboard motor 1 extends both horizontally and in a front to back direction. The front to back direction, the lateral direction, and the vertical direction in the following description correspond, respectively, to the front to back direction, the lateral direction, and the vertical direction when theoutboard motor 1 is in the basic posture. - The
outboard motor 1 includes an outboard motormain body 10 and an installation mechanism (not shown) arranged to install the outboard motormain body 10 on a hull (not shown). Supported by the installation mechanism, the outboard motormain body 10 is turned vertically about a laterally extendinghorizontal axis 11 and also turned laterally about a vertically extendingvertical axis 12. The outboard motormain body 10 includes thepropeller 2, anengine 13, adrive shaft 14, apropeller shaft 15, agear mechanism 16, acasing 17, a mount 18 (seeFIG. 2 below), and anengine cover 19. - The
engine 13 is, for example, an internal combustion engine or an electric motor. In this preferred embodiment, theengine 13 is preferably an internal combustion engine with a crankshaft (not shown) incorporated therein arranged to rotate about a vertically extending crank axis. Thedrive shaft 14 is coupled to a lower end of the crankshaft (not shown) of theengine 13 and extends downward. - The
propeller shaft 15 extends in in a front to back direction at a position lower than that of the lower end of thedrive shaft 14. Thegear mechanism 16 couples the lower end of thedrive shaft 14 and a front end of thepropeller shaft 15. Thepropeller 2 is attached to a rear end of thepropeller shaft 15. The rotation of thedrive shaft 14 with the driving of theengine 13 is transmitted by thegear mechanism 16 to thepropeller shaft 15. This allows thepropeller 2 to be driven and rotated by theengine 13. Therotation axis 2A of thepropeller 2 coincides with the central axis of thepropeller shaft 15. The rotation of thepropeller 2 generates a propulsive force for forward or rearward movement of the hull. - The
casing 17 is a vertically extending hollow body housing thedrive shaft 14, thepropeller shaft 15, and thegear mechanism 16 therein. Thepropeller shaft 15 and thegear mechanism 16 are housed in alower case 17A that is a lower end of thecasing 17. Thepropeller 2 is located outside thelower case 17A. -
FIG. 2 is a schematic exploded perspective view of an upper portion of the outboard motormain body 10. Themount 18 is a so-called exhaust guide preferably made of metal such as aluminum and having a plate shape. Themount 18 is installed in an upper end of thecasing 17 in a manner closing the interior space of thecasing 17 from above. The upper surface of themount 18 preferably has a rectangular or substantially rectangular shape elongated in the front to back direction. Theengine 13 is mounted on the upper surface of themount 18. Theouter edge 18A of the upper surface of themount 18 defines the outline of themount 18 in plan view and protrudes outwardly from theengine 13 around the entire circumference. - An
insertion hole 18B, anexhaust hole 18C located, for example, rearward of theinsertion hole 18B, and twodrainage holes 18D located, for example, on each of the left and right sides of theexhaust hole 18C are provided in the upper surface of themount 18. Theinsertion hole 18B, theexhaust hole 18C, and the drainage holes 18D penetrate through themount 18 vertically. Thedrive shaft 14 is inserted through theinsertion hole 18B. Exhaust gas from theengine 13 is discharged through theexhaust hole 18C and the interior of thecasing 17 out of the outboard motormain body 10. Water, if on the upper surface of themount 18, falls through thedrainage holes 18D and the interior of thecasing 17 to be discharged out of the outboard motormain body 10. It is noted that themount 18 may include a portion of a flow path for cooling water that cools theengine 13 or lubricant that lubricates theengine 13. - The
engine cover 19 preferably has a box shape and is located at a position higher than that of thecasing 17 to cover the engine 13 (seeFIG. 1 ). Theengine cover 19 is vertically divisible into atop portion 25 exemplifying a first cover and abottom portion 26. Thebottom portion 26 defining a lower portion of theengine cover 19 is divisible into at least afront bottom portion 27 exemplifying a second cover and aside bottom portion 28 exemplifying a third cover. - The
top portion 25 is made of, for example, resin and preferably has a box shape. Thetop portion 25 includes an opening (not shown) that opens the interior space thereof downward. In this preferred embodiment, the resin is preferably, for example, a thermosetting resin. Thelower edge 25A of thetop portion 25 has a continuous annular shape to define the opening. - The
front bottom portion 27 is made of, for example, metal such as aluminum and integrally includes ahorizontal portion 27A and avertical portion 27B. Thehorizontal portion 27A preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the vertical direction. Thehorizontal portion 27A preferably has a semicircular or substantially semicircular shape in plan view. The front edge of thehorizontal portion 27A is thus curved in an arcuate shape bulging forward. The rear edge of thehorizontal portion 27A is also curved in an arcuate shape bulging forward. The rear edge of thehorizontal portion 27A includes afitting groove 27C extending in a curved manner along the rear edge. Thefitting groove 27C is recessed forward and opens rearward. At positions adjacent to thefitting groove 27C in lateral ends of thehorizontal portion 27A, drainage holes 27D are provided in a manner vertically penetrating through thehorizontal portion 27A. - The
vertical portion 27B preferably has a plate shape curved along the front edge of thehorizontal portion 27A and extending upward. The front surface of thevertical portion 27B defines a portion of the outer surface of theengine cover 19. In an upper end of the front surface of thevertical portion 27B, there is ahorizontal step 27E extending laterally in a curved manner and a pair of left and rightvertical steps 27F extending downward from the lateral ends of thehorizontal step 27E. The portion of thevertical portion 27B higher than thehorizontal step 27E includes anupper end 27G of thefront bottom portion 27. The front surface of theupper end 27G is offset rearward by one step from the portion of the front surface of thevertical portion 27B surrounded by thehorizontal step 27E and the pair ofvertical steps 27F. Opposingportions 27H are provided integrally at the respective lateral ends of theupper end 27G. Ascrew hole 27I is provided in the left surface of the left opposingportion 27H. Ascrew hole 27I is also provided in the right surface of the right opposingportion 27H. The portion of thevertical portion 27B rearward of eachvertical step 27F will be referred to as arear portion 27J. The upper end edge of therear portion 27J is inclined so as to descend as it extends rearward. - The
side bottom portion 28 is made of, for example, resin and includes a pair of left and right portions. Of the pair of left and rightside bottom portions 28, the left sidebottom portion 28 will be referred to as a sidebottom portion 28L, while the rightside bottom portion 28 will be referred to as a sidebottom portion 28R. The sidebottom portion 28L and the sidebottom portion 28R are preferably laterally symmetric. Eachside bottom portion 28 integrally includes a plate-shapedmain body 28A extending in a front to back and vertical direction and anextended portion 28B extending in a manner bent from the rear end of themain body 28A toward the other sidebottom portion 28. The pair of sidebottom portions 28 are coupled through a right end of theextended portion 28B of the sidebottom portion 28L and a left end of theextended portion 28B of the sidebottom portion 28R. The right end of theextended portion 28B of the sidebottom portion 28L and the left end of theextended portion 28B of the sidebottom portion 28R will each be referred to as acoupling 28C. - In the side
bottom portion 28L, the left surface of themain body 28A and the rear surface of theextended portion 28B defines the outer surface of the sidebottom portion 28L and a portion of the outer surface of theengine cover 19. In the sidebottom portion 28L, the right surface of themain body 28A and the front surface of theextended portion 28B define the inner surface of the sidebottom portion 28L and a portion of the inner surface of theengine cover 19. In the sidebottom portion 28R, the right surface of themain body 28A and the rear surface of theextended portion 28B define the outer surface of the sidebottom portion 28R and a portion of the outer surface of theengine cover 19. In the sidebottom portion 28R, the left surface of themain body 28A and the front surface of theextended portion 28B define the inner surface of the sidebottom portion 28R and a portion of the inner surface of theengine cover 19. - In an upper end of the outer surface of each
side bottom portion 28, astep 28D extends from the front end of themain body 28A to thecoupling 28C. The portion of eachside bottom portion 28 higher than thestep 28D is anupper end 28E of theside bottom portion 28. The outer surface of theupper end 28E is offset by one step inside theengine cover 19 farther than the portion of the outer surface of theside bottom portion 28 lower than thestep 28D. In a front end of theupper end 28E, arecess 28F is recessed inward of theengine cover 19. Abottom portion 28G of therecess 28F is raised in a convex shape on the inner surface of theside bottom portion 28. Thebottom portion 28G is provided with aninsertion hole 28H penetrating laterally through thebottom portion 28G. - On the inner surface of each
side bottom portion 28, there is integrally provided an upper rib 28I protruding inward of theengine cover 19 and extending from the lower end of thebottom portion 28G of therecess 28F to the lower end of thecoupling 28C. On the inner surface of eachside bottom portion 28, there is integrally provided alower rib 28J extending from a location rearward of thebottom portion 28G to the lower end of thecoupling 28C. Thelower rib 28J is located below a portion of the upper rib 28I and extends parallel or substantially parallel with the upper rib 28I to the lower end of thecoupling 28C. Afitting groove 28K is provided between the upper rib 28I and thelower rib 28J. Thefitting groove 28K extends from a position rearward of thebottom portion 28G to the lower end of thecoupling 28C. The portion of the upper rib 28I located forward of thefitting groove 28K and extending to the lower end of therecess 28F will be referred to as anextended section 28M. Thelower rib 28J does not exist below theextended section 28M. - Assembly of the
divisible engine cover 19 will be described with reference also toFIG. 1 . First, an operator brings thefront bottom portion 27 closer to themount 18 and fits the front portion of theouter edge 18A of themount 18 into thefitting groove 27C in thehorizontal portion 27A of thefront bottom portion 27 from behind. This causes thefront bottom portion 27 to be coupled to themount 18. It is noted that the rear edge of thehorizontal portion 27A is provided with a fixedportion 27P protruding rearward to overlap the front end of themount 18 from above. A fastening member (not shown) such as a bolt is assembled into ascrew hole 18E in the front end of themount 18 through aninsertion hole 27Q defined in the fixedportion 27P such that themount 18 and thefront bottom portion 27 are fixed to each other. - Next, the operator arranges the pair of side
bottom portions 28 at a position rearward of thefront bottom portion 27 and sandwiches themount 18 bilaterally with theside bottom portions 28 until thecouplings 28C are coupled to each other. Then, the left portion of theouter edge 18A of themount 18 fits into thefitting groove 28K (not shown) in the sidebottom portion 28L from the right, while the right portion of theouter edge 18A fits into thefitting groove 28K in the sidebottom portion 28R from the left. This causes theside bottom portions 28 to be coupled to themount 18. It is noted that theside bottom portions 28 and themount 18 may be fixed using a fastening member such as a bolt if needed. - The front portion of the
main body 28A of the sidebottom portion 28L covers the leftrear portion 27J of thevertical portion 27B of thefront bottom portion 27 from the left. The front portion of themain body 28A of the sidebottom portion 28R covers the rightrear portion 27J of themain body 28A from the right. In this state, the left and right opposingportions 27H in theupper end 27G of thefront bottom portion 27 are opposed from within theengine cover 19 to thebottom portions 28G of therecesses 28F in the upper ends 28E of theside bottom portions 28 located at laterally corresponding positions. In addition, the insertion holes 28H in thebottom portions 28G and the screw holes 27I in the opposingportions 27H are aligned with each other. When the operator assemblescoupling members 29 such as bolts through the insertion holes 28H into the screw holes 27I, the opposingportions 27H and theside bottom portions 28 are coupled. This causes thefront bottom portion 27 and theside bottom portions 28 to be fixed to each other. - With the pair of side
bottom portions 28 being coupled to thefront bottom portion 27, thehorizontal step 27E of thevertical portion 27B of thefront bottom portion 27 and thesteps 28D of theside bottom portions 28 are connected to define one annular body (seeFIG. 1 ). The outer surface of theupper end 27G of thefront bottom portion 27 and the outer surfaces of the upper ends 28E of theside bottom portions 28 are also connected to define one annular body. Thefitting groove 27C in thehorizontal portion 27A of thefront bottom portion 27 and thefitting grooves 28K in theside bottom portions 28 are also connected to define one annular body. The upper end edges of the left and rightrear portions 27J of thevertical portion 27B are opposed from below to theextended sections 28M of theside bottom portions 28 located at laterally corresponding positions. - The operator then covers the
engine 13 with thetop portion 25. Thelower edge 25A of thetop portion 25 then encompasses the annular body defined by theupper end 27G of thefront bottom portion 27 and the upper ends 28E of theside bottom portions 28. This causes thetop portion 25 to be coupled to thefront bottom portion 27 and theside bottom portions 28. It is noted that thetop portion 25 may be fixed to thefront bottom portion 27 and theside bottom portions 28 using a fastening member such as a bolt if needed. - The assembling of the
engine cover 19 and the coupling of theengine cover 19 to themount 18 are thus completed. In the completedengine cover 19, thefront bottom portion 27 is located at a position lower than that of thetop portion 25 and the pair of sidebottom portions 28 are located at a position lower than that of thetop portion 25 and rearward of the front bottom portion 27 (seeFIG. 1 ). Theengine 13 mounted on themount 18 is opposed at least upward to thetop portion 25 and opposed forward to at least thevertical portion 27B of thefront bottom portion 27. Theengine 13 is also opposed sideward, that is, leftward and rightward to at least themain body portions 28A and opposed rearward to at least theextended portions 28B of the pair of sidebottom portions 28. Theengine cover 19 may further include arear panel 30 that covers theextended portions 28B of the pair of sidebottom portions 28 from behind. - A boundary exists between the
mount 18 and theengine cover 19 and multiple boundaries exist also in theengine cover 19 itself. The multiple boundaries in theengine cover 19 are, for example, one between thetop portion 25 and thefront bottom portion 27 and ones between the two portions of thefront bottom portion 27 and each side bottom portion 28 (referred to as a second boundary B2; seeFIG. 20 below). The boundary between thetop portion 25 and eachside bottom portion 28 and the boundary between the pair of sidebottom portions 28 also exist as boundaries in theengine cover 19. An air-intake structure (not shown) of theengine 13 including, for example, an air-intake box and a throttle body is located at a position within theengine cover 19 higher than those of the boundary between thetop portion 25 and thefront bottom portion 27 and the boundary between thetop portion 25 and eachside bottom portion 28. The boundary spanning the three portions of thetop portion 25, thefront bottom portion 27, and each side bottom portion 28 (referred to as a first boundary B1; seeFIG. 1 ) also exists as a boundary in theengine cover 19. The first boundary B1 and the second boundary B2 are continuous with each other. There further exists a boundary spanning the three portions of themount 18, thefront bottom portion 27, and eachside bottom portion 28. Theoutboard motor 1 includes a sealingstructure 40 that seals all of these boundaries.FIG. 3 is a perspective view of the sealingstructure 40. - The sealing
structure 40 includes afirst seal 41, asecond seal 42, athird seal 43, and afourth seal 44. Thefourth seal 44, thethird seal 43, thesecond seal 42, and thefirst seal 41 will hereinafter be described in this order. - The
fourth seal 44 preferably has a vertically extending columnar shape between thecouplings 28C of the pair of sidebottom portions 28. The cross-section of thefourth seal 44 in the direction perpendicular or substantially perpendicular to the direction in which thefourth seal 44 extends has a structure shown inFIG. 4 at any position in the extending direction of thefourth seal 44. Thefourth seal 44 includes acore portion 44A made of, for example, metal such as iron and anelastic portion 44B made of, for example, rubber and coating theentire core portion 44A. Thecore portion 44A preferably has a U-shaped or substantially U-shaped cross-section and theelastic portion 44B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to thecore portion 44A. It is noted that in this preferred embodiment, the rubber is, for example, a thermoplastic elastomer. Theelastic portion 44B includes a tongue-shapedfirst protrusion 44D protruding into aconcave space 44C sandwiched between thecore portion 44A. Thefirst protrusion 44D is provided on one of a pair of flat regions of the inner surface of theelastic portion 44B extending parallel or substantially parallel to each other with thespace 44C sandwiched therebetween and protrudes in a manner away from anopening 44E of thespace 44C. Multiplefirst protrusions 44D may be provided and, in this preferred embodiment, twofirst protrusions 44D are arranged parallel or substantially parallel to each other. Theelastic portion 44B includes asecond protrusion 44F protruding in a direction away from theopening 44E of thespace 44C. Thesecond protrusion 44F is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from theopening 44E. The curved portion of thecore portion 44A is positioned between thespace 44C and thesecond protrusion 44F. -
FIG. 5 is a schematic horizontal cross-sectional view of theengine cover 19 in the region A ofFIG. 3 . As for thefourth seal 44, thecoupling 28C of eachside bottom portion 28 preferably has a columnar shape protruding forward from the rear surface of theextended portion 28B and extending in the vertical direction. In eachcoupling 28C of eachside bottom portion 28, a vertically extendinggroove 28N is provided in a region opposing theother coupling 28C. Thegrooves 28N of each other's sidebottom portions 28 abut each other and are integral. One of the side bottom portions 28 (sidebottom portion 28L in this preferred embodiment) is only provided integrally with arib 28P protruding from the bottom of thegroove 28N and extending in the vertical direction. - The
fourth seal 44 spans thegrooves 28N of both sidebottom portions 28. In this state, therib 28P of the sidebottom portion 28L is fitted in thespace 44C of thefourth seal 44. In thefourth seal 44, theelastic portion 44B surrounds therib 28P and thefirst protrusion 44D in the front to back direction and is deformed in a manner following therib 28P and, in this state, adheres tightly to therib 28P. Thesecond protrusion 44F is also deformed in a manner sandwiched between the leading end of therib 28P and the bottom of thegroove 28N in the sidebottom portion 28R to adhere tightly to the bottom of thegroove 28N. This causes the boundary between thecouplings 28C of the pair of sidebottom portions 28 to be sealed entirely in the vertical direction by thefourth seal 44. - The
third seal 43 preferably has an annular shape extending along the annular body defined by thefitting groove 27C in thefront bottom portion 27 and thefitting grooves 28K in the side bottom portions 28 (seeFIGS. 2 and 3 ). The cross-section of thethird seal 43 in the direction perpendicular or substantially perpendicular to the direction in which thethird seal 43 extends has a structure shown inFIG. 6 at any position in the extending direction of thethird seal 43. Thethird seal 43 includes acore portion 43A made of, for example, metal and anelastic portion 43B made of, for example, rubber and coating theentire core portion 43A. Thecore portion 43A preferably has a U-shaped or substantially U-shaped cross-section and theelastic portion 43B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to thecore portion 43A. Theelastic portion 43B includes a tongue-shapedfirst protrusion 43D protruding into aconcave space 43C sandwiched between thecore portion 43A. Thefirst protrusion 43D is provided on one of a pair of flat regions of the inner surface of theelastic portion 43B extending parallel or substantially parallel to each other with thespace 43C sandwiched therebetween and protrudes in a manner away from anopening 43E of thespace 43C. Multiplefirst protrusions 43D may be provided and, in this preferred embodiment, twofirst protrusions 43D are arranged parallel or substantially parallel to each other. Theelastic portion 43B includes asecond protrusion 43F protruding in a direction away from theopening 43E of thespace 43C. Thesecond protrusion 43F preferably has a circular cross-section, for example. The curved portion of thecore portion 43A is positioned between thespace 43C and thesecond protrusion 43F. -
FIG. 7 is a schematic vertical cross-sectional rear view of theengine cover 19 in the region B ofFIG. 3 . Thethird seal 43 spans thefitting groove 27C in thefront bottom portion 27 and thefitting groove 28K in each side bottom portion 28 (thefitting groove 28K in the sidebottom portion 28L inFIG. 7 ). In this state, theouter edge 18A of themount 18 is fitted in thespace 43C of thethird seal 43. In thethird seal 43, theelastic portion 43B vertically sandwiches theouter edge 18A and thefirst protrusion 43D is deformed in a manner following theouter edge 18A and, in this state, adheres tightly to theouter edge 18A from above. Thesecond protrusion 43F is also deformed in a manner sandwiched between theouter edge 18A and the bottoms of the respectivefitting grooves mount 18 and thefront bottom portion 27 and the boundary between themount 18 and eachside bottom portion 28 to be sealed together around the entire circumference of theouter edge 18A by thethird seal 43. - The
second seal 42 includes a secondlower seal 46 and a second upper seal 47 (seeFIG. 3 ). The secondlower seal 46 preferably has an annular shape extending along the annular body defined by theupper end 27G of thefront bottom portion 27 and the upper ends 28E of theside bottom portions 28. The cross-section of the secondlower seal 46 in the direction perpendicular or substantially perpendicular to the direction in which the secondlower seal 46 extends has a structure shown inFIG. 8 at any position in the extending direction of the secondlower seal 46. - The second
lower seal 46 includes acore portion 46A made of, for example, metal and anelastic portion 46B made of, for example, rubber and coating theentire core portion 46A. Thecore portion 46A preferably has a vertically inverted U-shaped or substantially U-shaped cross-section and theelastic portion 46B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to thecore portion 46A. Theconcave space 46C sandwiched between thecore portion 46A opens downward. Theelastic portion 46B includes a tongue-shapedfirst protrusion 46D protruding upward into thespace 46C. Thefirst protrusion 46D is provided on one of a pair of flat regions (right flat region inFIG. 8 ) of the inner surface of theelastic portion 46B extending parallel or substantially parallel to each other with thespace 46C sandwiched therebetween and protrudes obliquely upward. Multiplefirst protrusions 46D may be provided and, in this preferred embodiment, twofirst protrusions 46D are arranged parallel or substantially parallel to each other. Theelastic portion 46B includes, on its side surface (left side surface inFIG. 8 ), asecond protrusion 46E protruding in a direction away from thespace 46C. The straight portion of thecore portion 46A is positioned between thespace 46C and thesecond protrusion 46E. Thesecond protrusion 46E is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from thespace 46C. - The second
upper seal 47 is made of, for example, rubber and preferably has a band shape extending along a portion of the second lower seal 46 (seeFIG. 3 ). The cross-section of the secondupper seal 47 in the direction perpendicular or substantially perpendicular to the direction in which the secondupper seal 47 extends has a structure shown inFIG. 9 at any position in the extending direction of the secondupper seal 47. The secondupper seal 47 integrally includes a fixedportion 47A and aprotrusion 47B. The fixedportion 47A preferably has a vertical plate shape.Adhesive 48 is provided on aside surface 47C of the fixedportion 47A. Theprotrusion 47B protrudes from theside surface 47D opposite to theside surface 47C of the fixedportion 47A. Theprotrusion 47B is hollow and preferably has a triangular or substantially triangular cross-section narrowing in the direction away from the side surfaces 47C and 47D. A pair ofconvex portions 47E protruding downward are provided at lower portions of theprotrusion 47B. One of theconvex portions 47E protrudes in a manner coming close to the fixedportion 47A as it extends downward, while the otherconvex portion 47E protrudes in a manner away from the fixedportion 47A as it extends downward. -
FIG. 10 is a schematic vertical cross-sectional rear view of theengine cover 19 in the region C ofFIG. 3 . Theupper end 27G of thefront bottom portion 27 and the upper ends 28E of the side bottom portions 28 (only theupper end 28E of the sidebottom portion 28L is shown inFIG. 10 ) are fitted in thespace 46C of the secondlower seal 46 from below. In the secondlower seal 46, theelastic portion 46B laterally sandwiches theupper end 28E and thefirst protrusion 46D is deformed in a manner following theupper end 28E and, in this state, laterally adheres tightly to theupper end 28E (from the right inFIG. 10 ). In addition, thesecond protrusion 46E is deformed in a manner hanging downward to adhere tightly to thelower edge 25A of thetop portion 25 from within theengine cover 19. This causes the boundary between thetop portion 25 and thefront bottom portion 27 and the boundary between thetop portion 25 and eachside bottom portion 28 to be sealed together around the entire circumference of thelower edge 25A by the secondlower seal 46. It is noted that thesecond protrusion 46E may adhere tightly to thelower edge 25A only laterally (seeFIGS. 16 and 20 below) or may adhere tightly to thelower edge 25A from below at theleading end 46F of thesecond protrusion 46E, as shown inFIG. 10 . - The second
upper seal 47 is located on a region rearward of the front portion of the secondlower seal 46 and preferably is U-shaped or substantially U-shaped in plan view (seeFIG. 3 ). The fixedportion 47A of the secondupper seal 47 follows the lower end of the inner surface of thetop portion 25 and is applied to thetop portion 25 via the adhesive 48. Theprotrusion 47B of the secondupper seal 47 is positioned over the secondlower seal 46 and adheres tightly to the secondlower seal 46 with the pair ofconvex portions 47E sandwiching an upper portion of the secondlower seal 46. This causes theclearance gap 49 sandwiched between the inner surface of thetop portion 25 and thesecond protrusion 46E of the secondlower seal 46 to be closed by the secondupper seal 47 from above and inhibits theclearance gap 49 from accumulating water therein. It is noted that since the secondlower seal 46 and the secondupper seal 47 are offset upward as they extend rearward (seeFIG. 3 ), theclearance gap 49 is also inclined. With this configuration, even if water enters theclearance gap 49, the water flows down through theclearance gap 49 and is discharged out of theclearance gap 49. - A pair of left and right first seals 41 are provided correspondingly to the pair of left and right side bottom portions 28 (see
FIG. 3 ). Of the pair of left and right first seals 41, the leftfirst seal 41 will be referred to as afirst seal 41L, while the rightfirst seal 41 will be referred to as afirst seal 41R. Thefirst seal 41L and thefirst seal 41R are preferably laterally symmetric. While thefirst seals 41 will hereinafter be described focusing on thefirst seal 41L, the following description of thefirst seal 41L, when reversed laterally, corresponds to description of thefirst seal 41R. -
FIG. 11 is a schematic perspective view of thefirst seal 41L. Thefirst seal 41L integrally includes afirst portion 51 exemplifying a three-part seal, asecond portion 52, and athird portion 53 exemplifying a two-part seal. Thefirst portion 51 is arranged at a position higher than that of thesecond portion 52 and thethird portion 53 extends from thefirst portion 51 to thesecond portion 52. Thefirst portion 51 and thesecond portion 52 are, for example, rubber molded articles and thethird portion 53 is a rubber extrusion molded article inserted in the molded articles. InFIG. 11 , the joint between thefirst portion 51 and thethird portion 53 and the joint between thesecond portion 52 and thethird portion 53 are respectively indicated by alternate long and short dashed lines. Thefirst portion 51, thesecond portion 52, and thethird portion 53 are preferably made of the same rubber material. Thefirst portion 51, thesecond portion 52, and thethird portion 53 will hereinafter be described in this order. - The
first portion 51 integrally includes aninner portion 51A and anouter portion 51B. Theinner portion 51A preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the lateral direction. The upper edge and the rear edge of theinner portion 51A are bent rightward. A pair of anteroposteriorvertical ribs 51C protruding leftward and extending vertically and parallel or substantially parallel to each other are provided in a front end of the left surface of theinner portion 51A. Of the pair ofvertical ribs 51C, the forwardvertical rib 51C may be referred to as a vertical rib 51CF, while the rearwardvertical rib 51C may be referred to as a vertical rib 51CR. The vertical rib 51CF defines a front edge of theinner portion 51A bent leftward. A vertically extendingwater storage groove 51D is located between and defined by the twovertical ribs 51C. - An
upper rib 51E protruding leftward is provided at a position of the left surface of theinner portion 51A below and adjacent to the upper edge. Theupper rib 51E is connected to the upper end of the vertical rib 51CF to close the upper end of thewater storage groove 51D and extends rearward from the upper end of thewater storage groove 51D to just before the rear edge of theinner portion 51A. A rear end of theupper rib 51E may be curved downward. Aguide 51F is provided in a lower end of the left surface of theinner portion 51A. Theguide 51F is a leftward protruding rib connected to a lower end of the vertical rib 51CF to close the lower end of thewater storage groove 51D and extends rearward from the lower end of thewater storage groove 51D to just before the rear edge of theinner portion 51A. Aninsertion hole 51G laterally penetrates a portion of theinner portion 51A that is rearward of thewater storage groove 51D and is vertically sandwiched between theupper rib 51E and theguide 51F. - The
inner portion 51A further includes anextended portion 51H extending leftward from the left end of theguide 51F and a lower rib 51I protruding leftward and upward from the boundary between theguide 51F and theextended portion 51H. Theextended portion 51H is connected to the lower end of the vertical rib 51CF and extends rearward behind theguide 51F. Arear portion 51J of theextended portion 51H is curved downward. A left end of therear portion 51J is bent downward. The lower rib 51I is connected to the lower end of the vertical rib 51CF and extends along theextended portion 51H. Adrainage groove 51K is located between and defined by theextended portion 51H and the lower rib 51I. Thedrainage groove 51K extends rearward from the lower end of the vertical rib 51CF to be curved downward and opens leftward. - The
outer portion 51B preferably has a plate shape with its thickness direction coinciding or substantially coinciding with the lateral direction and inclined with respect to theinner portion 51A in plan view so as to be offset rightward as it extends forward. Anupper end 51L of theouter portion 51B protrudes upward above theinner portion 51A. The upper end edge of theouter portion 51B is inclined so as to be offset downward as it extends forward. Therear edge 51M of theouter portion 51B is bent rightward. An upper end of therear edge 51M defines a portion of theupper end 51L. The upper end of therear edge 51M protrudes upward above the vertical rib 51CF of theinner portion 51A, and a portion of therear edge 51M lower than the upper end is connected to the vertical rib 51CF from the left. Thelower edge 51N of theouter portion 51B is bent leftward. A rear end of thelower edge 51N is bent downward and connected to the lower end of the vertical rib 51CF from the left. Therear edge 51M and the rear end of thelower edge 51N may be considered to be a portion of the vertical rib 51CF or the vertical rib 51CF may be considered to be a portion of therear edge 51M and thelower edge 51N. Thewater storage groove 51D in theinner portion 51A is adjacent to therear edge 51M from behind. - The
second portion 52 preferably has a box shape and its interior space opens downward. Thesecond portion 52 preferably has a triangular or substantially triangulartop surface 52A, and afront surface 52B, a sealingsurface 52C, and atapered surface 52D extending downward from the three respective sides of thetop surface 52A. Thesecond portion 52 also includes a pressedsurface 52E sandwiched between the sealingsurface 52C and the taperedsurface 52D. - The
top surface 52A extends horizontally or substantially horizontally. Thefront surface 52B extends in or substantially in the lateral direction. A vertically extendingpositioning groove 52F is provided at a lateral intermediate position of thefront surface 52B. Thepositioning groove 52F penetrates vertically through thesecond portion 52. Aprotrusion 52G defining the upper end of thepositioning groove 52F and protruding upward is provided on thetop surface 52A. The horizontal cross-section of theprotrusion 52G preferably is U-shaped or substantially U-shaped narrowing rearward. A rear end of theprotrusion 52G is the leading end of theprotrusion 52G and is preferably hollow. The interior space in the leading end of theprotrusion 52G defines anoutlet 52H (seeFIG. 17 below) opening downward from the interior space of thesecond portion 52. - A projection 52I protruding upward is provided on the
top surface 52A. The projection 52I extends rearward from the leading end of theprotrusion 52G to be bent leftward. The sealingsurface 52C is connected to the right end edge of thefront surface 52B and inclined so as to offset rearward as it extends leftward in plan view. The sealingsurface 52C may be flat or curved in a manner recessed forward in plan view. The taperedsurface 52D is connected to the left end edge of thefront surface 52B and inclined so as to offset downward as it extends leftward. The rear end of the upper end edge of the taperedsurface 52D is connected to the left end of the upper end edge of the sealingsurface 52C. A lower end of the taperedsurface 52D may be a vertical surface. The left end of the projection 52I is positioned at approximately the center of the upper end edge of the taperedsurface 52D. The pressedsurface 52E is bridged between the left end edge of the sealingsurface 52C and the rear end edge of the taperedsurface 52D and preferably has a triangular or substantially triangular shape widening downward. The pressedsurface 52E is inclined so as to offset forward as it extends leftward in plan view. - The
third portion 53 preferably has a columnar shape extending front to back between thefirst portion 51 and thesecond portion 52 in a manner inclined with respect to the horizontal direction. The cross-section of thethird portion 53 in the direction perpendicular or substantially perpendicular to the direction in which thethird portion 53 extends has a structure shown inFIG. 12 at any position in the extending direction of thethird portion 53. The thus simply shapedthird portion 53 having the same cross-section at any position is different in structure from thefirst portion 51 and thesecond portion 52 having their respective complex shapes. - The
third portion 53 includes acore portion 53A made of, for example, metal and anelastic portion 53B made of, for example, rubber and coating theentire core portion 53A. Thecore portion 53A preferably has a vertically inverted U-shaped or substantially U-shaped cross-section and theelastic portion 53B also preferably has a U-shaped or substantially U-shaped cross-section corresponding to thecore portion 53A. Theconcave space 53C sandwiched between thecore portion 53A opens downward. A front end of theelastic portion 53B is connected to therear portion 51J of theextended portion 51H and the lower rib 51I of thefirst portion 51, while a rear end of theelastic portion 53B is connected to theprotrusion 52G of the second portion 52 (seeFIG. 11 ). - The
elastic portion 53B includes a tongue-shapedfirst protrusion 53D protruding leftward and upward in thespace 53C. Thefirst protrusion 53D is provided on one of a pair of left and right flat regions (right flat region inFIG. 12 ) of the inner surface of theelastic portion 53B extending parallel or substantially parallel to each other with thespace 53C sandwiched therebetween. Multiplefirst protrusions 53D may be provided and, in this preferred embodiment, twofirst protrusions 53D are arranged parallel or substantially parallel to each other. A concavo-convex portion 53F defined by alternating concaves and convexes is provided vertically on the other one 53E of the pair of left and right flat regions (left flat region inFIG. 12 ) of the inner surface of theelastic portion 53B. - The
elastic portion 53B includes asecond protrusion 53G protruding upward from an upper end of thecore portion 53A. Thesecond protrusion 53G is hollow and preferably has a triangular or substantially triangular cross-section narrowing upward. The interior space of thesecond protrusion 53G defines aflow path 53H connected to thedrainage groove 51K in the first portion 51 (seeFIG. 11 ) and theoutlet 52H of the second portion 52 (seeFIG. 17 ). -
FIG. 13 is a schematic left side view of thefirst seal 41L and its periphery. InFIG. 13 , thefront bottom portion 27 and the secondlower seal 46 are shown as the periphery. Thefirst seal 41L is arranged along the left opposingportion 27H in theupper end 27G of thefront bottom portion 27 and the upper end edge of the leftrear portion 27J of thevertical portion 27B. Thefirst portion 51, thesecond portion 52, and thethird portion 53 of thefirst seal 41L in this state will hereinafter be described in this order. -
FIG. 14 is an end view of a cut portion along the line A-A inFIG. 13 . At least a portion of theinner portion 51A of thefirst portion 51 is located between the left opposingportion 27H in thefront bottom portion 27 and thebottom portion 28G of therecess 28F in theupper end 28E of the sidebottom portion 28L. A raisedportion 27K raised outward (leftward inFIG. 14 ) in a manner encompassing thescrew hole 27I is provided on the outer surface (left surface inFIG. 14 ) of the opposingportion 27H. The raisedportion 27K is fitted in theinsertion hole 51G in thefirst portion 51 with no clearance gap. Ascrew portion 29A of thecoupling member 29 that couples the opposingportion 27H and the sidebottom portion 28L is assembled into thescrew hole 27I while being inserted through theinsertion hole 51G. Between ahead portion 29B of thecoupling member 29 and the raisedportion 27K, there is interposed acylindrical collar 60 encompassing thescrew portion 29A and acylindrical grommet 61 fitted in theinsertion hole 28H in thebottom portion 28G while encompassing thecollar 60. By way of example, thecollar 60 is preferably made of metal, while thegrommet 61 is preferably made of resin. A peripheral portion of theinsertion hole 28H in the sidebottom portion 28L is fitted entirely with no clearance gap in afitting groove 61A provided in the outer peripheral surface of thegrommet 61. - The upper edge of the
inner portion 51A is engaged with the opposingportion 27H from above, while the rear edge of theinner portion 51A is engaged with the opposingportion 27H from behind. In theinner portion 51A, the vertical rib 51CR, theupper rib 51E, and the lower rib 51I protrude toward theupper end 28E of the sidebottom portion 28L and adhere tightly to the inner surface of the sidebottom portion 28L. Specifically, the vertical rib 51CR and theupper rib 51E extend leftward to adhere tightly to the right surface of thebottom portion 28G in theupper end 28E, while the lower rib 51I is deformed in a manner following the lower surface of thebottom portion 28G to adhere tightly to the lower surface of thebottom portion 28G. Accordingly, theclearance gap 62 between the opposingportion 27H and thebottom portion 28G is closed by the vertical rib 51CR from the front and also closed by theupper rib 51E and the lower rib 51I from above and below to be opened only rearward. Thewater storage groove 51D in theinner portion 51A, which is positioned forward of the vertical rib 51CR, is opposed to theupper end 28E of the sidebottom portion 28L (particularly a region of the right surface of thebottom portion 28G forward of theinsertion hole 28H). -
FIG. 15 is a schematic perspective view of thefirst portion 51 and its periphery. InFIG. 15 , thefront bottom portion 27 and the sidebottom portion 28L are shown as the periphery. Theouter portion 51B of thefirst portion 51 is arranged on the outer surface of theupper end 27G of thefront bottom portion 27, and therear edge 51M of theouter portion 51B closes the boundary between the outer surface of theupper end 27G of thefront bottom portion 27 and the outer surface of theupper end 28E of the sidebottom portion 28L. That is, theouter portion 51B is arranged on the outer surface of theupper end 27G of thefront bottom portion 27 through the boundary. It is noted that therear edge 51M in this state is not compressed between thefront bottom portion 27 and the sidebottom portion 28L and therefore cannot resist against the movement of the sidebottom portion 28L during its application or removal. This allows the operator to apply and remove the sidebottom portion 28L smoothly. Thelower edge 51N of theouter portion 51B is arranged along a left rear end of thehorizontal step 27E and an upper end of the leftvertical step 27F. -
FIG. 16 is an end view of a cut portion along the line B-B inFIG. 13 . As mentioned above, the boundary between thetop portion 25 and thefront bottom portion 27 and the boundary between thetop portion 25 and eachside bottom portion 28 are sealed together by the secondlower seal 46. Theelastic portion 46B of the secondlower seal 46 sandwiching theupper end 27G of thefront bottom portion 27 sandwiches theupper end 51L, which is a portion of theouter portion 51B, between the same and the outer surface of theupper end 27G. - Accordingly, the first boundary B1 between the
top portion 25, thefront bottom portion 27, and the sidebottom portion 28L is sealed by both thefirst portion 51 and the secondlower seal 46. -
FIG. 17 is a cross-sectional view taken along the line C-C inFIG. 13 .FIG. 18 is an end view of a cut portion along the line D-D inFIG. 13 .FIG. 19 is a cross-sectional view taken along the line E-E inFIG. 18 . A right portion of thesecond portion 52 is housed in a left end of thefitting groove 27C in the front bottom portion 27 (see alsoFIG. 2 ). The sealingsurface 52C of thesecond portion 52 is smoothly continuous with a region (not shown) of the bottom of thefitting groove 27C adjoining thesecond portion 52 from the right. The sealingsurface 52C of thesecond portion 52 in this state adheres tightly to thesecond protrusion 43F of thethird seal 43 from the front and left at the boundary between thefront bottom portion 27, themount 18, and the sidebottom portion 28L. Thepositioning groove 52F and a portion of thesecond portion 52 to the left of thepositioning groove 52F stick out leftward from thefitting groove 27C. A rear end of the leftrear portion 27J in thevertical portion 27B of thefront bottom portion 27 will be referred to as apositioning portion 27L. Thepositioning portion 27L is fitted in thepositioning groove 52F from the front (seeFIG. 17 ). - A pair of upper and lower
horizontal walls 27M extending rearward parallel or substantially parallel to each other and avertical wall 27N extending upward from the front end of the lowerhorizontal wall 27M are provided on the rear edge of thehorizontal portion 27A of the front bottom portion (seeFIG. 19 ). Thefitting groove 27C in thefront bottom portion 27 defines a space between the pair ofhorizontal walls 27M and thevertical wall 27N defines the bottom of thefitting groove 27C. Thesecond portion 52, which is partially housed in thefitting groove 27C, is sandwiched vertically between the pair ofhorizontal walls 27M and in contact with thevertical wall 27N from behind. This causes thesecond portion 52 to be positioned vertically and anteroposteriorly. The projection 52I on thetop surface 52A of thesecond portion 52 adheres tightly to the upperhorizontal wall 27M. - The front region of the
fitting groove 28K in eachside bottom portion 28 is deeper than the rear region (see thefitting groove 28K in the sidebottom portion 28R inFIG. 2 ). In this regard, theengine cover 19 further includes a raisedportion 63 to be attached to each side bottom portion 28 (seeFIG. 17 ). The raisedportion 63 is, for example, a hollow body, which is housed in the front region of thefitting groove 28K to raise the front region of thefitting groove 28K. This fills the gap between theouter surface 28Q of theside bottom portion 28 defining a design surface and theouter edge 18A of themount 18. - The raised
portion 63 includes a sealingsurface 63A continuous with the sealingsurface 52C of thesecond portion 52 and the bottom (not shown) of the rear region of thefitting groove 28K, and apressing surface 63B bent from the front end of the sealingsurface 63A to extend laterally outward (leftward in the case of the sidebottom portion 28L) in an inclined manner. The sealingsurface 63A adheres tightly to thesecond protrusion 43F of thethird seal 43 from the left. Thepressing surface 63B presses against the pressedsurface 52E of thesecond portion 52 from the left and behind. This causes thesecond portion 52 to be urged so as to come close to thesecond protrusion 43F, according to the mutual inclination between thepressed surface 52E and thepressing surface 63B, and a reaction force from thesecond protrusion 43F onto thesecond portion 52 to be generated. Since the reaction force allows to maintain an adequate sealing margin between the sealingsurface 52C and thesecond protrusion 43F, the sealingsurface 52C and thesecond protrusion 43F adhere to each other very tightly. - Of the upper rib 28I and the
lower rib 28J vertically sandwiching thefitting groove 28K in eachside bottom portion 28, the upper rib 28I protrudes inside theengine cover 19 farther inward than thelower rib 28J to be placed on thetop surface 52A of the second portion 52 (seeFIG. 18 ). The sidebottom portion 28L is attached to thefront bottom portion 27 from the left. Upon this, the upper rib 28I of the sidebottom portion 28L is guided by the taperedsurface 52D of thesecond portion 52 to be placed smoothly on thetop surface 52A. The projection 52I on thetop surface 52A adheres tightly not only to the upperhorizontal wall 27M of thefitting groove 27C in thefront bottom portion 27 as mentioned above, but also to the upper rib 28I (seeFIGS. 18 and 19 ). This causes the clearance gap between thefitting groove 27C and thefitting groove 28K to be closed by the projection 52I. - Accordingly, the boundary between the
front bottom portion 27, themount 18, and the sidebottom portion 28L is sealed by both thesecond portion 52 and thethird seal 43. It is noted that the upperhorizontal wall 27M is provided with avertical wall 27R (see alsoFIG. 2 ) with its thickness direction coinciding or substantially coinciding with the lateral direction, and thevertical wall 27R adjoins the boundary between thefront bottom portion 27, themount 18, and the sidebottom portion 28L from the right. This allows thevertical wall 27R to prevent external water from entering into theengine cover 19 through the boundary as a sheet of spray. -
FIG. 20 is an end view of a cut portion along the line F-F inFIG. 13 . As for thefirst seal 41L, the upper end of the leftrear portion 27J of thefront bottom portion 27 is fitted in thespace 53C in thethird portion 53 from below. In thethird portion 53, theelastic portion 53B laterally sandwiches the upper end of therear portion 27J and thefirst protrusion 53D is deformed in a manner following the upper end of therear portion 27J and, in this state, laterally adheres tightly to therear portion 27J (from the right inFIG. 20 ). The concavo-convex portion 53F (see alsoFIG. 12 ) of theelastic portion 53B, which is positioned opposite to thefirst protrusion 53D with respect to therear portion 27J, is also compressed between the upper end of therear portion 27J and thecore portion 53A to adhere tightly to therear portion 27J. Further, thesecond protrusion 53G of thethird portion 53 is deformed in a manner sandwiched between therear portion 27J and theextended section 28M of the sidebottom portion 28L to adhere tightly to theextended section 28M from below. This causes the second boundary B2 between thefront bottom portion 27 and the sidebottom portion 28L to be sealed by thethird portion 53 entirely in the front to back direction. The leading end 53I of thesecond protrusion 53G is continuous with the lower rib 51I of thefirst portion 51 and the projection 52I of thesecond portion 52. Thefirst seal 41 is therefore provided with asingle seal line 54 defined by theupper rib 51E, the vertical rib 51CR, and the lower rib 51I of thefirst portion 51, the projection 52I of thesecond portion 52, and the leading end 53I of the third portion 53 (seeFIG. 11 ). The boundary between thefront bottom portion 27 and the sidebottom portion 28L is sealed along theseal line 54. - In accordance with the preferred embodiments described above, the
engine cover 19 is divisible into three or more divided covers including thetop portion 25, thefront bottom portion 27, and the side bottom portions 28 (seeFIG. 2 ). Theengine cover 19 thus includes the boundary (first boundary B1) between thetop portion 25, thefront bottom portion 27, and theside bottom portions 28 and the boundary between thefront bottom portion 27, themount 18, and theside bottom portions 28. - The
first seal 41L of the sealingstructure 40 seals the boundary (first boundary B1) between thetop portion 25, thefront bottom portion 27, and the sidebottom portion 28L with the first portion 51 (seeFIGS. 14 to 16 ). Thefirst seal 41L seals the boundary between thefront bottom portion 27, themount 18, and the sidebottom portion 28L with the second portion 52 (seeFIGS. 17 to 19 ). Thefirst seal 41L seals the other boundary (the second boundary B2 between thefront bottom portion 27 and the sidebottom portion 28L) extending between these boundaries with the third portion 53 (seeFIG. 20 ). - The
first seal 41R of the sealingstructure 40 seals the boundary (first boundary B1) between thetop portion 25, thefront bottom portion 27, and the sidebottom portion 28R with thefirst portion 51 and seals the boundary between thefront bottom portion 27, themount 18, and the sidebottom portion 28R with thesecond portion 52. Thefirst seal 41R seals the other boundary (the second boundary B2 between thefront bottom portion 27 and the sidebottom portion 28R) extending between these boundaries with thethird portion 53. - The
second seal 42 of the sealingstructure 40 provides desirable sealing characteristics at the boundary between thetop portion 25 and thefront bottom portion 27 and the boundary between thetop portion 25 and each side bottom portion 28 (seeFIG. 10 ). Thethird seal 43 of the sealingstructure 40 provides desirable sealing characteristics at the boundary between themount 18 and thefront bottom portion 27 and the boundary between themount 18 and each side bottom portion 28 (seeFIG. 7 ). Thefourth seal 44 of the sealingstructure 40 seals the boundary between the pair of side bottom portions 28 (seeFIG. 5 ). - As described heretofore, it is possible to provide desirable sealing characteristics of the
divisible engine cover 19 having such a complex structure. This significantly reduces or prevents external water from entering into theengine 13 through the boundaries between the multiple divided covers in theengine cover 19. - In the
first seal 41, thefirst portion 51 seals theclearance gap 62 between the opposingportion 27H in theupper end 27G of thefront bottom portion 27 and theupper end 28E of eachside bottom portion 28 with theinner portion 51A (seeFIG. 14 ). Further, thefirst portion 51 seals the boundary between the outer surface of theupper end 27G of thefront bottom portion 27 and the outer surface of theupper end 28E of eachside bottom portion 28 with therear edge 51M of theouter portion 51B (seeFIG. 15 ). This provides desirable sealing characteristics at the boundary between theupper end 27G of thefront bottom portion 27 and theupper end 28E of eachside bottom portion 28. This significantly reduces or prevents external water from leaking through the boundary between theupper end 28E of eachside bottom portion 28 and theupper end 27G of thefront bottom portion 27 and entering into theengine 13. - Since the
inner portion 51A is arranged in a manner offset by one step inside theengine cover 19 farther inward than theouter portion 51B, external water is less likely to reach theinner portion 51A through the boundary between the outer surface of theupper end 27G of thefront bottom portion 27 and the outer surface of theupper end 28E of theside bottom portion 28. Even if external water leaks through the boundary between the outer surface of theupper end 27G of thefront bottom portion 27 and the outer surface of theupper end 28E of eachside bottom portion 28 and enters into theengine cover 19, the water is immediately contained in thewater storage groove 51D in theinner portion 51A. It is therefore difficult for the water to reach theengine 13. This further significantly reduces or prevents water from entering into theengine 13. - The interior of the
engine cover 19 has a negative pressure due to the air-intake by theengine 13. Water within thewater storage groove 51D therefore tends to scatter toward the air-intake structure (not shown) upward and taken into theengine 13. However, the water within thewater storage groove 51D is blocked by theupper rib 51E from scattering upward within theengine cover 19 to reach theengine 13, which further significantly reduces or prevents water from entering into theengine 13. - Water within the
water storage groove 51D slides on theguide 51F (seeFIG. 11 ) to be guided rearward by theguide 51F. This causes the water to fall out of theguide 51F to be guided into thedrainage hole 27D in theengine cover 19 and/or thedrainage hole 18D in the mount 18 (seeFIG. 2 ) and eventually discharged out of theengine cover 19, which further significantly reduces or prevents water from entering into theengine 13. - Even if external water reaches the
insertion hole 51G and enters theclearance gap 62 between the opposingportion 27H of theinner portion 51A of thefront bottom portion 27 and eachside bottom portion 28, the water is blocked by theupper rib 51E from scattering upward to reach theengine 13. Further, the water is guided by theguide 51F into thedrainage hole 27D and thedrainage hole 18D to be discharged out of theengine cover 19. This further significantly reduces or prevents water from entering into theengine 13. - External water may reach not the
water storage groove 51D or theinsertion hole 51G but thedrainage groove 51K (seeFIG. 11 ) within theinner portion 51A. In this case, water within thedrainage groove 51K flows through theflow path 53H within thesecond protrusion 53G of the third portion 53 (seeFIG. 20 ) to flow down through theoutlet 52H of the second portion 52 (seeFIG. 17 ) downward from thesecond portion 52 to be discharged through thedrainage hole 27D in theengine cover 19 and/or thedrainage hole 18D in themount 18. - The
second seal 42 sandwiches theupper end 51L of theouter portion 51B, which seals the boundary between the outer surface of theupper end 27G of thefront bottom portion 27 and the outer surface of theupper end 28E of eachside bottom portion 28 in thefirst seal 41, between the same and the front bottom portion 27 (seeFIG. 16 ). This causes thefirst seal 41 and thesecond seal 42 to be continuous with each other. Since the boundary (first boundary B1) between thetop portion 25, thefront bottom portion 27, and eachside bottom portion 28 is thus sealed by both thefirst seal 41 and thesecond seal 42, desirable sealing characteristics are provided at the boundary. This significantly reduces or prevents external water from leaking through the boundary and entering into theengine 13. - In the
first seal 41, the sealingsurface 52C of thesecond portion 52 adheres tightly to thethird seal 43 from the front at the boundary between thefront bottom portion 27, themount 18, and eachside bottom portion 28 to seal the boundary (seeFIG. 17 ). This causes thefirst seal 41 and thethird seal 43 to be continuous with each other. Since the boundary is thus sealed by both thefirst seal 41 and thethird seal 43, desirable sealing characteristics are provided at the boundary. This significantly reduces or prevents external water from leaking through the boundary and entering into theengine 13. - The
second portion 52 may be positioned laterally by thepositioning groove 52F and thepositioning portion 27L to seal the boundary between thefront bottom portion 27, themount 18, and eachside bottom portion 28 with the lateral position being stabilized. This provides desirable sealing characteristics at the boundary and thus significantly reduces or prevents external water from leaking through the boundary and entering into theengine 13. - In the thus arranged
first seal 41, thefirst portion 51 and thesecond portion 52 are preferably molded articles, while thethird portion 53 is preferably an extrusion molded article, which makes it possible to achieve the structure in which thefirst seal 41 integrally includes thefirst portion 51, thesecond portion 52, and thethird portion 53. The clearance gap at the complex first boundary B1 spanning the three portions of thetop portion 25, thefront bottom portion 27, and eachside bottom portion 28 is filled with thefirst portion 51, which is a molded article. Further, the clearance gap at the complex boundary spanning the three portions of thefront bottom portion 27, themount 18, and eachside bottom portion 28 is filled with thesecond portion 52, which is also a molded article. The clearance gap at the relatively simple second boundary B2 spanning the two portions of thefront bottom portion 27 and eachside bottom portion 28 is filled with thethird portion 53, which is an extrusion molded article. This allows thefirst seal 41 to seal together the boundaries. - Although the preferred embodiments of the present invention have been described above, the present invention is not restricted to the contents of these preferred embodiments and various modifications are possible within the scope of the present invention.
- For example, only one of the pair of side
bottom portions 28 may be provided separately and the other sidebottom portion 28 may be integral with thetop portion 25 or thefront bottom portion 27. In this case, only one first seal 31 may also be provided correspondingly to the separate sidebottom portion 28. - Also, features of two or more of the various preferred embodiments described above may be combined.
- While preferred embodiments of the present invention have been described above, it is to be understood that variations and modifications will be apparent to those skilled in the art without departing from the scope and spirit of the present invention. The scope of the present invention, therefore, is to be determined solely by the following claims.
Claims (20)
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JP2017-095809 | 2017-05-12 | ||
JP2017095809A JP6815272B2 (en) | 2017-05-12 | 2017-05-12 | Seal structure for outboard motors and split engine covers used for them |
Publications (2)
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US20180327067A1 true US20180327067A1 (en) | 2018-11-15 |
US10286990B2 US10286990B2 (en) | 2019-05-14 |
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US15/964,137 Active US10286990B2 (en) | 2017-05-12 | 2018-04-27 | Outboard motor and sealing structure for divisible engine cover used therefor |
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JP (1) | JP6815272B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20220204148A1 (en) * | 2020-12-28 | 2022-06-30 | Yamaha Hatsudoki Kabushiki Kaisha | Outboard motor engine cover and outboard motor |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2021146921A (en) * | 2020-03-19 | 2021-09-27 | 本田技研工業株式会社 | Seal structure |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4348194A (en) * | 1980-07-01 | 1982-09-07 | Brunswick Corporation | Cowl for an outboard motor |
US4723927A (en) * | 1986-08-20 | 1988-02-09 | Brunswick Corporation | Marine drive outboard engine cowl |
US4800854A (en) * | 1987-07-24 | 1989-01-31 | Brunswick Corporation | Cowl assembly for an outboard motor |
US5069643A (en) | 1990-05-18 | 1991-12-03 | Outboard Marine Corporation | Molded lower motor cover |
US5360358A (en) * | 1993-05-21 | 1994-11-01 | Outboard Marine Corporation | Hidden lower motor cover attachment means |
US5487687A (en) * | 1994-07-18 | 1996-01-30 | Brunswick Corporation | Midsection and cowl assembly for an outboard marine drive |
JPH10175594A (en) * | 1996-12-19 | 1998-06-30 | Honda Motor Co Ltd | Outboard engine |
US6663450B1 (en) * | 2002-06-14 | 2003-12-16 | Brunswick Corporation | Integral cowl latching mechanism for an outboard motor |
US6669517B1 (en) * | 2002-06-14 | 2003-12-30 | Brunswick Corporation | Multiple part cowl structure for an outboard motor |
CA2584386C (en) * | 2006-05-01 | 2013-11-19 | Honda Motor Co., Ltd. | Outboard engine unit |
-
2017
- 2017-05-12 JP JP2017095809A patent/JP6815272B2/en active Active
-
2018
- 2018-04-27 US US15/964,137 patent/US10286990B2/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20220204148A1 (en) * | 2020-12-28 | 2022-06-30 | Yamaha Hatsudoki Kabushiki Kaisha | Outboard motor engine cover and outboard motor |
US11760458B2 (en) * | 2020-12-28 | 2023-09-19 | Yamaha Hatsudoki Kabushiki Kaisha | Outboard motor engine cover and outboard motor |
Also Published As
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JP2018192840A (en) | 2018-12-06 |
US10286990B2 (en) | 2019-05-14 |
JP6815272B2 (en) | 2021-01-20 |
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